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618: 1819: 697: 1853: 1657:(nar) Safety Code, model rockets are constructed of paper, wood, plastic and other lightweight materials. The code also provides guidelines for motor use, launch site selection, launch methods, launcher placement, recovery system design and deployment and more. Since the early 1960s, a copy of the Model Rocket Safety Code has been provided with most model rocket kits and motors. Despite its inherent association with extremely flammable substances and objects with a pointed tip traveling at high speeds, model rocketry historically has proven to be a very safe hobby and has been credited as a significant source of inspiration for children who eventually become 3894: 4754:"If you have ever seen a big fire hose spraying water, you may have noticed that it takes a lot of strength to hold the hose (sometimes you will see two or three firefighters holding the hose). The hose is acting like a rocket engine. The hose is throwing water in one direction, and the firefighters are using their strength and weight to counteract the reaction. If they were to let go of the hose, it would thrash around with tremendous force. If the firefighters were all standing on skateboards, the hose would propel them backward at great speed!" 2795: 271: 3624: 3122: 453: 1943:) acting on that part of the combustion chamber. In a properly designed engine, the flow will reach Mach 1 at the throat of the nozzle. At which point the speed of the flow increases. Beyond the throat of the nozzle, a bell shaped expansion part of the engine allows the gases that are expanding to push against that part of the rocket engine. Thus, the bell part of the nozzle gives additional thrust. Simply expressed, for every action there is an equal and opposite reaction, according to 2161: 3401: 1399: 1550: 1915: 4262: 1317: 1116: 8627: 4463: 4293: 42: 3141:, which improves the performance of flights. The higher the ratio, the less engine mass is needed to be carried. This permits the carrying of even more propellant, enormously improving the delta-v. Alternatively, some rockets such as for rescue scenarios or racing carry relatively little propellant and payload and thus need only a lightweight structure and instead achieve high accelerations. For example, the Soyuz escape system can produce 20  1225: 8638: 555: 4477: 1951: 1985:. Because a rocket, propellant and exhaust in flight, without any external perturbations, may be considered as a closed system, the total momentum is always constant. Therefore, the faster the net speed of the exhaust in one direction, the greater the speed of the rocket can achieve in the opposite direction. This is especially true since the rocket body's mass is typically far lower than the final total exhaust mass. 423: 4449: 3409: 735:, where a V-2 is exhibited in the main exhibition hall, states: "The V-2 was a quantum leap of technological change. We got to the Moon using V-2 technology but this was technology that was developed with massive resources, including some particularly grim ones. The V-2 programme was hugely expensive in terms of lives, with the Nazis using slave labour to manufacture these rockets". In parallel with the German 1473: 1719: 871: 1927:
produces thrust against the ambient environment to which these gases are released. The ideal direction of motion of the exhaust is in the direction so as to cause thrust. At the top end of the combustion chamber the hot, energetic gas fluid cannot move forward, and so, it pushes upward against the top of the rocket engine's
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However, as speeds rise, the resultant exhaust speed goes down, and the overall vehicle energetic efficiency rises, reaching a peak of around 100% of the engine efficiency when the vehicle is travelling exactly at the same speed that the exhaust is emitted. In this case the exhaust would ideally stop
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that can be used with rockets come surprisingly close: when the nozzle expands the gas, the gas is cooled and accelerated, and an energy efficiency of up to 70% can be achieved. Most of the rest is heat energy in the exhaust that is not recovered. The high efficiency is a consequence of the fact that
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generated 180 dB of noise around its base. To combat this, NASA developed a sound suppression system which can flow water at rates up to 900,000 gallons per minute (57 m/s) onto the launch pad. The water reduces the noise level from 180 dB down to 142 dB (the design requirement is
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Most of the takeoff mass of a rocket is normally propellant. However propellant is seldom more than a few times more expensive than gasoline per kilogram (as of 2009 gasoline was about $ 1/kg  or less), and although substantial amounts are needed, for all but the very cheapest rockets, it turns
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This fact is used in interplanetary travel. It means that the amount of delta-v to reach other planets, over and above that to reach escape velocity can be much less if the delta-v is applied when the rocket is travelling at high speeds, close to the Earth or other planetary surface; whereas waiting
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by it. Using a convergent/divergent nozzle gives more force since the exhaust also presses on it as it expands outwards, roughly doubling the total force. If propellant gas is continuously added to the chamber then these pressures can be maintained for as long as propellant remains. Note that in the
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of such a vehicle would make its useful payload tiny or nonexistent. Most current and historical launch vehicles "expend" their jettisoned hardware, typically by allowing it to crash into the ocean, but some have recovered and reused jettisoned hardware, either by parachute or by propulsive landing.
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The energy density of a typical rocket propellant is often around one-third that of conventional hydrocarbon fuels; the bulk of the mass is (often relatively inexpensive) oxidizer. Nevertheless, at take-off the rocket has a great deal of energy in the fuel and oxidizer stored within the vehicle. It
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In a closed chamber, the pressures are equal in each direction and no acceleration occurs. If an opening is provided in the bottom of the chamber then the pressure is no longer acting on the missing section. This opening permits the exhaust to escape. The remaining pressures give a resultant thrust
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Noise is generally most intense when a rocket is close to the ground, since the noise from the engines radiates up away from the jet, as well as reflecting off the ground. This noise can be reduced somewhat by flame trenches with roofs, by water injection around the jet and by deflecting the jet at
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that provides stable support until a few seconds after ignition. Due to their high exhaust velocity—2,500 to 4,500 m/s (9,000 to 16,200 km/h; 5,600 to 10,100 mph)—rockets are particularly useful when very high speeds are required, such as orbital speed at approximately 7,800 m/s
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Illustration of the pendulum rocket fallacy. Whether the motor is mounted at the bottom (left) or top (right) of the vehicle, the thrust vector (T) points along an axis that is fixed to the vehicle (top), rather than pointing vertically (bottom) independent of vehicle attitude, which would lead the
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Almost all of a launch vehicle's mass consists of propellant. Mass ratio is, for any 'burn', the ratio between the rocket's initial mass and its final mass. Everything else being equal, a high mass ratio is desirable for good performance, since it indicates that the rocket is lightweight and hence
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allowable for weight reasons. Components produced in small numbers if not individually machined can prevent amortization of R&D and facility costs over mass production to the degree seen in more pedestrian manufacturing. Amongst liquid-fueled rockets, complexity can be influenced by how much
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of the combustion of propellant in the rocket engine is to increase the internal energy of the resulting gases, utilizing the stored chemical energy in the fuel. As the internal energy increases, pressure increases, and a nozzle is used to convert this energy into a directed kinetic energy. This
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The aerospace giants shared almost $ 500 million in equity profits from the rocket-making venture last year, when it still had a monopoly on the business of blasting the Pentagon's most important satellites into orbit. But since then, 'They've had us on a very short leash,' Tory Bruno, United
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As the remaining propellant decreases, rocket vehicles become lighter and their acceleration tends to increase until the propellant is exhausted. This means that much of the speed change occurs towards the end of the burn when the vehicle is much lighter. However, the thrust can be throttled to
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is more or less the speed the exhaust leaves the vehicle, and in the vacuum of space, the effective exhaust velocity is often equal to the actual average exhaust speed along the thrust axis. However, the effective exhaust velocity allows for various losses, and notably, is reduced when operated
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of 0.7, a rocket flying at Mach 0.85 (which most aircraft cruise at) with an exhaust velocity of Mach 10, would have a predicted overall energy efficiency of 5.9%, whereas a conventional, modern, air-breathing jet engine achieves closer to 35% efficiency. Thus a rocket would need about 6x more
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Peak accelerations can be increased by designing the vehicle with a reduced mass, usually achieved by a reduction in the fuel load and tankage and associated structures, but obviously this reduces range, delta-v and burn time. Still, for some applications that rockets are used for, a high peak
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Once above the majority of the atmosphere, the vehicle then angles the rocket jet, pointing it largely horizontally but somewhat downwards, which permits the vehicle to gain and then maintain altitude while increasing horizontal speed. As the speed grows, the vehicle will become more and more
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by Hermann Oberth, who became the film's scientific adviser and later an important figure in the team that developed the V-2 rocket. The film was thought to be so realistic that it was banned by the Nazis when they came to power for fear it would reveal secrets about the V-2 rockets.
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Hobbyists build and fly a wide variety of model rockets. Many companies produce model rocket kits and parts but due to their inherent simplicity some hobbyists have been known to make rockets out of almost anything. Rockets are also used in some types of consumer and professional
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dead in space behind the moving vehicle, taking away zero energy, and from conservation of energy, all the energy would end up in the vehicle. The efficiency then drops off again at even higher speeds as the exhaust ends up traveling forwards – trailing behind the vehicle.
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is a type of model rocket using water as its reaction mass. The pressure vessel (the engine of the rocket) is usually a used plastic soft drink bottle. The water is forced out by a pressurized gas, typically compressed air. It is an example of Newton's third law of motion.
1006:, but to make an efficient, accurate rocket or missile involves overcoming a number of difficult problems. The main difficulties include cooling the combustion chamber, pumping the fuel (in the case of a liquid fuel), and controlling and correcting the direction of motion. 551:." The patent "Improvements in Rockets" was raised in July 1918 but not published until February 1923 for security reasons. Firing and guidance controls could be either wire or wireless. The propulsion and guidance rocket eflux emerged from the deflecting cowl at the nose. 2386:(integral of mass and velocity) of the object. As such, it is the best performance class (payload mass and terminal velocity capability) indicator of a rocket, rather than takeoff thrust, mass, or "power". The total impulse of a rocket (stage) burning its propellant is: 1592:. This is a small, usually solid rocket that is capable of pulling the crewed capsule away from the main vehicle towards safety at a moments notice. These types of systems have been operated several times, both in testing and in flight, and operated correctly each time. 4147:
energy; and allowing for the specific energy of rocket propellant being around one third that of conventional air fuel, roughly 18x more mass of propellant would need to be carried for the same journey. This is why rockets are rarely if ever used for general aviation.
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of 30,000 km/h. At this altitude and velocity, the vehicle had a kinetic energy of about 3 TJ and a potential energy of roughly 200 GJ. Given the initial energy of 20 TJ, the Space Shuttle was about 16% energy efficient at launching the orbiter.
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are common, primarily from engineering, fabrication, and testing; raw materials amount to typically around 2% of total expense. For most rockets except reusable ones (shuttle engines) the engines need not function more than a few minutes, which simplifies design.
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In May 2003 the astronaut office made clear its position on the need and feasibility of improving crew safety for future NASA crewed missions indicating their "consensus that an order of magnitude reduction in the risk of human life during ascent, compared to the
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The maximum speeds that can be achieved with staging is theoretically limited only by the speed of light. However the payload that can be carried goes down geometrically with each extra stage needed, while the additional delta-v for each stage is simply additive.
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The rate of propellant flow through a rocket engine is often deliberately varied over a flight, to provide a way to control the thrust and thus the airspeed of the vehicle. This, for example, allows minimization of aerodynamic losses and can limit the increase of
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hardware must be lightweight, like pressure-fed engines can have two orders of magnitude lesser part count than pump-fed engines but lead to more weight by needing greater tank pressure, most often used in just small maneuvering thrusters as a consequence.
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Drag is a force opposite to the direction of the rocket's motion relative to any air it is moving through. This slows the speed of the vehicle and produces structural loads. The deceleration forces for fast-moving rockets are calculated using the
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For crewed rockets various methods are used to reduce the sound intensity for the passengers, and typically the placement of the astronauts far away from the rocket engines helps significantly. For the passengers and crew, when a vehicle goes
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145 dB). Without the sound suppression system, acoustic waves would reflect off of the launch pad towards the rocket, vibrating the sensitive payload and crew. These acoustic waves can be so severe as to damage or destroy the rocket.
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The shape of the nozzle is important. Consider a balloon propelled by air coming out of a tapering nozzle. In such a case the combination of air pressure and viscous friction is such that the nozzle does not push the balloon but is
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Le macchine cifrate di Giovanni Fontana: con la riproduzione del Cod. icon. 242 della Bayerische Staatsbibliothek di Monaco di Baviera e la decrittazione di esso e del Cod. lat. nouv. acq. 635 della Bibliothèque nationale di
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first proposed the concept of using rockets to enable human spaceflight in 1861. Leitch's rocket spaceflight description was first provided in his 1861 essay "A Journey Through Space", which was later published in his book
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is determined by measurement while testing the engine. In practice the effective exhaust velocities of rockets varies but can be extremely high, ~4500 m/s, about 15 times the sea level speed of sound in air.
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out that the propellant costs are usually comparatively small, although not completely negligible. With liquid oxygen costing $ 0.15 per kilogram ($ 0.068/lb) and liquid hydrogen $ 2.20/kg ($ 1.00/lb), the
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part of the rocket engine nozzle on the high pressure fluid of combustion gases, is to cause the gases to accelerate to high speed. The higher the speed of the gases, the lower the pressure of the gas (
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The costs of rockets can be roughly divided into propellant costs, the costs of obtaining and/or producing the 'dry mass' of the rocket, and the costs of any required support equipment and facilities.
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in 2009 had a liquid propellant expense of approximately $ 1.4 million for each launch that cost $ 450 million from other expenses (with 40% of the mass of propellants used by it being liquids in the
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The costs of support equipment, range costs and launch pads generally scale up with the size of the rocket, but vary less with launch rate, and so may be considered to be approximately a fixed cost.
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of about 10, and achieved a specific impulse of 263 seconds. This gives a delta-v of around 5.9 km/s whereas around 9.4 km/s delta-v is needed to achieve orbit with all losses allowed for.
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fired its engines for around 8.5 minutes, consuming 1,000 tonnes of solid propellant (containing 16% aluminium) and an additional 2,000,000 litres of liquid propellant (106,261 kg of
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case of liquid propellant engines, the pumps moving the propellant into the combustion chamber must maintain a pressure larger than the combustion chamber—typically on the order of 100 atmospheres.
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The scale of amateur rocketry can range from a small rocket launched in one's own backyard to a rocket that reached space. Amateur rocketry is split into three categories according to total engine
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A typical rocket engine can handle a significant fraction of its own mass in propellant each second, with the propellant leaving the nozzle at several kilometres per second. This means that the
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The energy density is 31MJ per kg for aluminum and 143 MJ/kg for liquid hydrogen, this means that the vehicle consumed around 5 TJ of solid propellant and 15 TJ of hydrogen fuel.
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of a rocket engine, and often the entire vehicle can be very high, in extreme cases over 100. This compares with other jet propulsion engines that can exceed 5 for some of the better engines.
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over land (or over a populated area, e.g. Russia usually does launch over land, but over unpopulated areas), or if the rocket is trying to reach an orbital plane that does not reach the
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from these shock waves depends on the size of the rocket as well as the exhaust velocity. The sound intensity of large, high performance rockets could potentially kill at close range.
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is about 9.7 km/s, which leaves the vehicle with a sideways speed of about 7.8 km/s at an altitude of around 200 km. In this manoeuvre about 1.9 km/s is lost in
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Achievable mass ratios are highly dependent on many factors such as propellant type, the design of engine the vehicle uses, structural safety margins and construction techniques.
873: 250:). Chemical rockets store a large amount of energy in an easily released form, and can be very dangerous. However, careful design, testing, construction and use minimizes risks. 3581:
of the rocket engine limits the maximum acceleration that can be designed. It turns out that rocket engines generally have truly excellent thrust to weight ratios (137 for the
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When launched from the Earth practical delta-vs for a single rockets carrying payloads can be a few km/s. Some theoretical designs have rockets with delta-vs over 9 km/s.
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To change the preceding factors for orbital launch vehicles, proposed methods have included mass-producing simple rockets in large quantities or on large scale, or developing
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Even though a rocket's non-propellant, dry mass is often only between 5–20% of total mass, nevertheless this cost dominates. For hardware with the performance used in orbital
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Rocket vehicles are often constructed in the archetypal tall thin "rocket" shape that takes off vertically, but there are actually many different types of rockets including:
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capacity of a rocket is the theoretical total change in velocity that a rocket can achieve without any external interference (without air drag or gravity or other forces).
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can be significant due to the path of the rocket around the center of a celestial body; when high enough speeds in the right direction and altitude are achieved a stable
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In a chemical propulsion device, the engine efficiency is simply the ratio of the kinetic power of the exhaust gases and the power available from the chemical reaction:
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As can be seen from the thrust equation, the effective speed of the exhaust controls the amount of thrust produced from a particular quantity of fuel burnt per second.
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A gallery of behind-the-scenes shots of movies featuring space travel or aliens. Page 68, photo caption: "Directed by Fritz Lang (third from right), the silent film "
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Extreme performance requirements for rockets reaching orbit correlate with high cost, including intensive quality control to ensure reliability despite the limited
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was at the top and the fuel tank at the bottom of the rocket, based on Goddard's belief that the rocket would achieve stability by "hanging" from the engine like a
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offset or vary this if needed. Discontinuities in acceleration also occur when stages burn out, often starting at a lower acceleration with each new stage firing.
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As a side effect, these pressures on the rocket also act on the exhaust in the opposite direction and accelerate this exhaust to very high speeds (according to
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are commonly used to carry instruments that take readings from 50 kilometers (31 mi) to 1,500 kilometers (930 mi) above the surface of the Earth. The
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Understanding force: an account of some aspects of teaching the idea of force in school, college and university courses in engineering, mathematics and science
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Understanding force: an account of some aspects of teaching the idea of force in school, college and university courses in engineering, mathematics and science
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to produce large volumes of very hot gas. The oxidiser is either kept separate and mixed in the combustion chamber, or comes premixed, as with solid rockets.
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later (in 1903) also conceived this idea, and extensively developed a body of theory that has provided the foundation for subsequent spaceflight development.
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Plot of instantaneous propulsive efficiency (blue) and overall efficiency for a rocket accelerating from rest (red) as percentages of the engine efficiency
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in 1814. Together, the Mysorean and British innovations increased the effective range of military rockets from 100 to 2,000 yards (91 to 1,829 m).
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the speed of the exhaust of a rocket determines how much momentum increase is created for a given amount of propellant. This is called the rocket's
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where high performance is less necessary, a pressurised fluid is used as propellant that simply escapes the spacecraft through a propelling nozzle.
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meant to fly very frequently to amortize their up-front expense over many payloads, or reducing rocket performance requirements by constructing a
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Since the energy ultimately comes from fuel, these considerations mean that rockets are mainly useful when a very high speed is required, such as
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A model rocket is a small rocket designed to reach low altitudes (e.g., 100–500 m (330–1,640 ft) for 30 g (1.1 oz) model) and
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Impulse is defined as a force acting on an object over time, which in the absence of opposing forces (gravity and aerodynamic drag), changes the
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Rocket launch technologies include the entire set of systems needed to successfully launch a vehicle, not just the vehicle itself, but also the
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low speed military applications where their low-speed inefficiency is outweighed by their extremely high thrust and hence high accelerations.
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of the launch site. Doglegs are undesirable due to extra onboard fuel required, causing heavier load, and a reduction of vehicle performance.
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rocket combustion can be performed at very high temperatures and the gas is finally released at much lower temperatures, and so giving good
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The required delta-v can also be calculated for a particular manoeuvre; for example the delta-v to launch from the surface of the Earth to
7063: 6200: 5514: 1130:. The rocket engines powering rockets come in a great variety of different types; a comprehensive list can be found in the main article, 7797: 6521: 4231:. This delta-v means that the speed increases (or decreases) by a particular amount, independent of the initial speed. However, because 7178: 5620: 7440: 5830: 5489: 4983:
Rockets appear in Arab literature in 1258 A.D., describing Mongol invaders' use of them on February 15 to capture the city of Baghdad
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A balloon with a tapering nozzle. The balloon is pushed by the higher pressure at the top than found around the inside of the nozzle.
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of these gases through the engine exerts force ("thrust") on the combustion chamber and nozzle, propelling the vehicle (according to
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dated to 1245. Internal-combustion rocket propulsion is mentioned in a reference to 1264, recording that the "ground-rat", a type of
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The Tsiolkovsky rocket equation gives a relationship between the mass ratio and the final velocity in multiples of the exhaust speed
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Space handbook: Astronautics and its applications : Staff report of the Select Committee on Astronautics and Space Exploration
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One subtle feature of rockets relates to energy. A rocket stage, while carrying a given load, is capable of giving a particular
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During a launch, as the vehicle speed increases, and the atmosphere thins, there is a point of maximum aerodynamic drag called
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of space. Rockets work more efficiently in a vacuum and incur a loss of thrust due to the opposing pressure of the atmosphere.
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is a dimensionless parameter that is identical to the acceleration of the rocket propulsion system (expressed in multiples of
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fuel) to lift the 100,000 kg vehicle (including the 25,000 kg payload) to an altitude of 111 km and an orbital
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Acoustic Prediction Methods for Rocket Engines, Including the Effects of Clustered Engines and Deflected Exhaust Flow, CR-566
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The reliability of rockets, as for all physical systems, is dependent on the quality of engineering design and construction.
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which would be able to reach orbit without staging, none have ever been constructed, and, if powered only by rockets, the
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with the result that the exiting gases produce the reaction of a force on the rocket causing it to accelerate the rocket.
7645: 7239: 7133: 7091: 6223: 6078: 6054: 4350:, is both achievable with current technology and consistent with NASA's focus on steadily improving rocket reliability". 1439: 814: 606:, highly directed jet of gas, more than doubling the thrust and raising the engine efficiency from 2% to 64%. His use of 497:(1813). In 1814, Congreve published a book in which he discussed the use of multiple rocket launching apparatus. In 1815 7805: 7339: 7112: 6387: 582: 7921: 4371: 2528: 486:
was referring, when he wrote of the "rockets' red glare" while held captive on a British ship that was laying siege to
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to the Middle East and to Europe in the mid-13th century. According to Joseph Needham, the Song navy used rockets in a
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The minimal mass of vehicle consists of a rocket engine with minimal fuel and structure to carry it. In that case the
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Corpulent Stump is the most powerful non-commercial rocket ever launched on an Aerotech engine in the United Kingdom.
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Sometimes the propellant is not burned but still undergoes a chemical reaction, and can be a 'monopropellant' such as
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For a more detailed model of the net thrust of a rocket engine that includes the effect of atmospheric pressure, see
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adopted the Italian term into German in the mid-16th century; "rocket" appears in English by the early 17th century.
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Some notable mass fractions are found in the following table (some aircraft are included for comparison purposes):
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into orbit and beyond. They are also used to rapidly accelerate spacecraft when they change orbits or de-orbit for
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serving as the technical director. The V-2 became the first artificial object to travel into space by crossing the
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designed an electrically steered rocket… Rocket experiments were conducted under my own patents with the help of
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and is used for the rocket to gain altitude and speed. However, much of the lost energy ends up in the exhaust.
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Thus far, the required velocity (delta-v) to achieve orbit has been unattained by any single rocket because the
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may usefully employ for propulsion, such as in space. In these circumstances, it is necessary to carry all the
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in 1804. This rocket was based directly on the Mysorean rockets, used compressed powder and was fielded in the
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until the rocket has slowed at altitude multiplies up the effort required to achieve the desired trajectory.
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For example, the first stage of the Saturn V, carrying the weight of the upper stages, was able to achieve a
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are used in many military aircraft to propel crew away to safety from a vehicle when flight control is lost.
17: 6308: 3065: 2072:) present will, unless deliberate control efforts are made, naturally cause the vehicle to follow a roughly 1852: 1357:
carrying their own propellant must be used when there is no other substance (land, water, or air) or force (
759:). The Allies' rocket programs were less technological, relying mostly on unguided missiles like the Soviet 688:
film critic Stephen Armstrong states Lang "created the rocket industry". Lang was inspired by the 1923 book
8037: 5702:
The Naval Institute guide to combat fleets of the world 2000–2001 : their ships, aircraft, and systems
4606: 4326:), consequences of accidents can be severe. Most space missions have some problems. In 1986, following the 1086: 367:
gave instructions for constructing devices that are similar to firecrackers based on second hand accounts.
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system for part of the velocity to orbit (or all of it but with most methods involving some rocket use).
3600:. For these operations to be done it is necessary for a vehicle's engines to provide more than the local 3296: 3151:
The highest mass ratios are generally achieved with liquid rockets, and these types are usually used for
2844: 2789: 1811: 1647: 1135: 1031: 460: 378: 7623: 6923: 6651: 1757:, are usually from a fixed location on the ground, but would also be possible from an aircraft or ship. 8521: 8290: 7963: 7314: 5725: 5075: 4235:
is a square law on speed, this means that the faster the rocket is travelling before the burn the more
3601: 3160: 2323: 1098: 516: 5068:"Transfer Of Islamic Technology To The West, Part III: Technology Transfer in the Chemical Industries" 5041: 3592:
The high accelerations that rockets naturally possess means that rocket vehicles are often capable of
3566:
is the net force acting on the rocket (mostly thrust, but air drag and other forces can play a part).
3163:), and these types are able to use lightweight, low pressure tanks and typically run high-performance 8444: 8326: 8064: 7829: 7772: 3802: 2504: 1780:
needed for a successful launch or recovery or both. These are often collectively referred to as the "
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Thus, the greater the specific impulse, the greater the net thrust and performance of the engine.
1537:. Also, a rocket may be used to soften a hard parachute landing immediately before touchdown (see 1058:) to hold these components together. Rockets intended for high speed atmospheric use also have an 238:), two liquids that must be ignited to react (like kerosene (RP1) and liquid oxygen, used in most 8563: 8499: 8278: 8180: 8091: 7995: 7968: 7869: 7650: 6345: 5860: 5770: 3787:{\displaystyle \eta _{c}={\frac {{\frac {1}{2}}{\dot {m}}v_{e}^{2}}{\eta _{combustion}P_{chem}}}} 2045: 1737: 950: 817:(ICBMs). The 1960s saw rapid development of rocket technology, particularly in the Soviet Union ( 642: 638: 296:
during this time. The Mongols adopted Chinese rocket technology and the invention spread via the
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in flight. However, the rocket veered off course and crashed 184 feet (56 m) away from the
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performs better, for essentially the same reasons that low weight is desirable in sports cars.
2459:
The total impulse of a multi-stage rocket is the sum of the impulses of the individual stages.
2188: 1940: 1765: 1447: 1435: 1298: 1171: 1119: 732: 525: 6166: 2294: 214:
are the most common type of high power rocket, typically creating a high speed exhaust by the
8461: 8268: 7906: 6410:"Demonstration of the flying rocket belt, Fort Eustis, Virginia and the Pentagon, 06/07/1961" 5900: 5893: 5765:
United States Congress. House Select Committee on Astronautics and Space Exploration (1959),
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commonly take off vertically, and then begin to progressively lean over, usually following a
1529:, which are used for many commercial purposes. Indeed, rockets remain the only way to launch 1526: 1345:, indicating that the rocket was no more stable than one with the rocket engine at the base. 1207: 1069:
As well as these components, rockets can have any number of other components, such as wings (
822: 235: 231: 5153: 2752: 2690: 2598: 2430: 2141:. This determines the minimum aerodynamic strength of the vehicle, as the rocket must avoid 8630: 8531: 8514: 8151: 8086: 8079: 7936: 7822: 7185: 5624: 4573: 4543: 4308: 4055: 3893: 3836: 3542: 2985: 2956: 2927: 2819: 2722: 2332: 1932: 1754: 1596: 1589: 1525:(28,000 km/h; 17,000 mph). Spacecraft delivered into orbital trajectories become 1294: 1195: 1167: 1094: 1023: 986: 795: 646: 626: 510: 412: 396: 197: 7447: 5928:. Reston, Virginia: American Institute of Aeronautics and Astronautics. pp. 267, 269. 5839: 5561: 8: 8526: 8504: 8439: 8158: 8002: 5490:"Woman in the Moon – Philip French on Fritz Lang's handsomely restored moon-mission yarn" 4971: 4591: 4576: – Rocket that burns 3 propellants at once or 2 fuels with an oxidizer, sequentially 4562: 4430: 4155: 2591:
An equivalent measure, the net impulse per weight unit of propellant expelled, is called
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Alternatively, an inert propellant can be used that can be externally heated, such as in
778:. After World War II scientists used rockets to study high-altitude conditions, by radio 775: 774:, including Wernher von Braun, in 1945, and brought them to the United States as part of 92: 74: 54: 7590: 6988: 5940: 2154: 1608: 1604: 441:
were the first successful iron-cased rockets, developed in the late 18th century in the
8672: 8641: 8424: 8350: 8205: 8101: 7953: 7396: 5422:"Katyusha rocket launcher. Weapon of Victory: multiple launch rocket system 'Katyusha'" 5109: 4817: 4482: 4434: 4367: 3951: 3931: 3474: 3442: 3404:
Spacecraft staging involves dropping off unnecessary parts of the rocket to reduce mass
2552: 1928: 1923: 1455: 1326: 671: 599: 548: 532: 259: 154: 100: 50: 7042: 6898: 6258: 6079:"Soyuz T-10-1 'Launch vehicle blew up on pad at Tyuratam; crew saved by abort system'" 2843:
is constant, the delta-v that a rocket vehicle can provide can be calculated from the
1959:
on the side opposite the opening, and these pressures are what push the rocket along.
1895:
the sound cuts off as the sound waves are no longer able to keep up with the vehicle.
1438:
use rocket engines to engage targets at high speed at a range of several miles, while
731:
on 20 June 1944. Doug Millard, space historian and curator of space technology at the
452: 8682: 8637: 8596: 8236: 8131: 8106: 8052: 8042: 7859: 7550: 7386: 6823: 6771: 6713: 6619: 6580: 6172: 6004: 5904: 5776: 5775:, House document / 86th Congress, 1st session, no. 86, Washington (DC): U.S. G.P.O., 5705: 5680: 5565: 5476: 5361: 5200: 5169: 5132: 5000: 4901: 4828: 4531: 4339: 4319: 3841: 3395: 2377: 1954:
Rocket thrust is caused by pressures acting on both the combustion chamber and nozzle
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Cold War submarines : the design and construction of U.S. and Soviet submarines
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Battisti, Eugenio; Saccaro Del Buffa Battisti, Giuseppa; Fontana, Giovanni (1984).
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Thus jet engines, with a better match between speed and jet exhaust speed (such as
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to their targets. A rocket and its payload together are generally referred to as a
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tank or casing, prior to being used as the propulsive mass that is ejected from a
1158:. Some rockets use heat or pressure that is supplied from a source other than the 8554: 8454: 8407: 8305: 8246: 8231: 8185: 8168: 8074: 8069: 7809: 7740: 7681: 7427: 7371:"Reliability and crew safety assessment for a solid rocket booster/J-2S launcher" 7013: 6817: 5646: 5554: 5316: 4942: 4895: 4708: 4674: 4468: 4454: 4411:
Rockets in applications other than launch to orbit (such as military rockets and
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has so far not been achievable, orbital rockets always have more than one stage.
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Great Mambo Chicken And The Transhuman Condition: Science Slightly Over The Edge
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The Rocket and the Reich: Peenemünde and the Coming of the Ballistic Missile Era
5098:"'The Soul of Artillery': Congreve's Rockets and Their Effectiveness in Warfare" 3623: 493:
The first mathematical treatment of the dynamics of rocket propulsion is due to
322:, also known as the Fire Drake Manual, written by the Chinese artillery officer 8601: 8588: 8481: 8412: 8402: 8387: 8365: 8355: 8251: 8241: 8190: 8111: 7370: 5348: 5063: 5029: 4378: 4236: 4232: 3852: 3644: 2101: 2089: 2035: 1857: 1788: 1781: 1773: 1585: 1554: 1451: 1139: 1039: 937: 929: 903: 842: 803: 736: 704: 577: 331: 313: 193: 146: 121:
from Earth and therefore can achieve unlimited maximum altitude. Compared with
84: 7382: 7243: 6735: 6409: 6050: 5870: 4690: – Vehicle or machine that is able to fly by gaining support from the air 4425:
Space launch market competition § 2010s: Competition and pricing pressure
3643:
is of course desirable that as much of the energy of the propellant end up as
3121: 164:
Rockets for military and recreational uses date back to at least 13th-century
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along a rail at extremely high speed. The world record for this is Mach 8.5.
1334: 1275: 1260: 1237: 1155: 1131: 1110: 1027: 982: 970: 826: 818: 813:
rockets became extremely important militarily with the development of modern
791: 748: 540: 501:
constructed rocket-launching platforms, which allowed rockets to be fired in
368: 353:), which included 107 gunpowder recipes, 22 of them for rockets. In Europe, 247: 189: 96: 7677:"The inside story of how billionaires are racing to take you to outer space" 6623: 6456: 5780: 4696: – The hypothesis that inertial and gravitational masses are equivalent 4570: – Thermal rocket that uses superheated water held in a pressure vessel 3847:
However, engine efficiency is not the whole story. In common with the other
3400: 602:. These nozzles turn the hot gas from the combustion chamber into a cooler, 8606: 8541: 8210: 8195: 7896: 7891: 5856: 5365: 4567: 4043:{\displaystyle \eta _{p}={\frac {2{\frac {u}{c}}}{1+({\frac {u}{c}})^{2}}}} 3655: 3052: 2105: 2077: 2041: 1837: 1792: 1674: 1641: 1549: 1398: 1290: 1203: 1182:. With combustive propellants a chemical reaction is initiated between the 1175: 1163: 1003: 915: 907: 850: 684: 654: 487: 364: 289: 126: 88: 7137: 7095: 6952: 6827: 5379: 2160: 1316: 433:
used to defeat an East India Company battalion during the Battle of Guntur
8434: 8300: 7990: 7973: 7845: 7781: 7116: 5193: 4714: 4668: 4534: – Structure built on a rocket launch pad to service launch vehicles 3453:, where rockets are burning together and then detach when they burn out. 1863:
Rocket exhaust generates a significant amount of acoustic energy. As the
1704: 1600: 1538: 1515: 1503: 1467: 1264: 1244: 1143: 1115: 1082: 1070: 1059: 991: 960: 919: 783: 536: 400: 373: 354: 318: 276: 227: 7155: 6112: 5113: 5097: 4261: 2130:(the "classic" rocket shape—long and thin), and by keeping the rocket's 280:: "fire arrow", "dragon-shaped arrow frame", and a "complete fire arrow" 8568: 8476: 8419: 8379: 8173: 7874: 7524:. Andrews Space and Technology (original figure source). Archived from 7369:
Fragola, J.; Baum, J.D.; Sauvageau, D.; Horowitz, S.J. (January 2006).
5968:"High Altitude Research at the Applied Physics Laboratory in the 1940s" 4625: 4382: 4292: 3848: 3435: 3420: 3370: 3315: 3185: 3164: 3138: 3116: 2006: 1892: 1868: 1864: 1769: 1700: 1530: 1521: 1496: 1425: 1374: 1342: 1233: 1191: 1127: 1078: 942: 799: 712: 700: 675: 661: 614:
greatly lowered the weight and increased the effectiveness of rockets.
603: 591: 359: 215: 125:, rockets are lightweight and powerful and capable of generating large 7315:"Going Private: The Promise and Danger of Space Travel By Tariq Malik" 4741: 3265:
104,000 kg + 28,800 kg (~230,000 lb + ~63,500 lb)
3245:
13,300 kg + 118,000 kg (~29,320 lb + ~260,150 lb)
1822:
Doglegged flight path of a PSLV launch to polar inclinations avoiding
1224: 8578: 8429: 8146: 8027: 7948: 7931: 6854: 4646: 4612: 4537: 4179: 3901:
From these principles it can be shown that the propulsive efficiency
3449:
where the rockets light after the previous stage has fallen away, or
3276: 3217: 2123: 2068: 1856:
Workers and media witness the Sound Suppression Water System test at
1696: 1670: 1658: 1424:(not all missiles use rocket engines, some use other engines such as 1362: 1271: 1074: 1063: 1055: 1051: 911: 880: 779: 679: 611: 554: 446: 416: 334:(Huo long chu shui), thought to have been used by the Chinese navy. 309: 285: 177: 173: 169: 103:
to exhaust expelled at high speed. Rocket engines work entirely from
41: 226:. The stored propellant can be a simple pressurized gas or a single 7755: 6489: 6461: 5473:. Los Angeles, California: Directors Guild of America, Inc.: 64–71. 5452: 4687: 4323: 4171: 3412: 3352: 3237: 3197: 3048: 2383: 2142: 2073: 1841: 1662: 1619: 1581: 1338: 1283: 1256: 1187: 976: 965: 933: 883: 854: 810: 787: 740: 728: 305: 223: 134: 130: 46: 6193:"N1 (vehicle 5L) moon rocket Test – launch abort system activated" 3206:
2,700 kg + 16,000 kg (~6,000 lb + ~35,300 lb)
1232:
Rocket propellant is mass that is stored, usually in some form of
6312: 5866: 5515:"Watch the Silent Film that Brought Rocket Science to the Masses" 4433:
for obtaining spaceflight services emerged, bringing substantial
4228: 3586: 3585:
engine; some solid rockets are over 1000), and nearly all really
2810: 2799: 2362: 2026: 1743: 1534: 1416: 1411: 1393: 1370: 1358: 1002:
A rocket design can be as simple as a cardboard tube filled with
924: 764: 422: 357:
mentioned firecrackers made in various parts of the world in the
323: 181: 158: 80: 7750: 7577:
U.S. Air Force Research Report No. AU-ARI-93-8: LEO On The Cheap
7375:
RAMS '06. Annual Reliability and Maintainability Symposium, 2006
6859:(Master's thesis). Air Force Institute of Technology. p. 2. 3574:
acceleration applied for just a short time is highly desirable.
3408: 1950: 1565:
Rockets were used to propel a line to a stricken ship so that a
1251:. For chemical rockets often the propellants are a fuel such as 8256: 4819:
Porcupine, Picayune, & Post: How Newspapers Get Their Names
2020: 1570: 1248: 1199: 1134:. Most current rockets are chemically powered rockets (usually 1043: 752: 634: 185: 108: 7814: 6287: 4677: – Rocket designed to take measurements during its flight 2951:
is the initial total mass, including propellant, in kg (or lb)
953:(including rocket-assisted takeoff of conventional aircraft – 316:. Subsequently, rockets are included in the military treatise 107:
carried within the vehicle; therefore a rocket can fly in the
7787: 3582: 2138: 2056: 2002: 1574: 1366: 1241: 590:). Modern rockets originated in 1926 when Goddard attached a 502: 382: 342: 165: 7798:
Relativity Calculator – Learn Tsiolkovsky's rocket equations
7368: 3137:
of any type of engine; and this helps vehicles achieve high
1799:
horizontal until at orbital speed, the engine will cut off.
782:
of temperature and pressure of the atmosphere, detection of
509:
in 1844 greatly increased the accuracy of rocket artillery.
326:
in the mid-14th century. This text mentions the first known
7733: 7728: 5729: 4999:. Cambridge: Cambridge University Press. pp. 100–103. 4412: 4159: 4151: 3597: 3333: 2803: 2566: 1806:, that is, jettison hardware on the way to orbit. Although 1183: 1035: 954: 830: 744: 385:
engineer in 1420, created rocket-propelled animal figures.
351:
The Book of Military Horsemanship and Ingenious War Devices
7760: 7745: 5129:
Rockets and missiles : the life story of a technology
5013: 4322:(greater energy by weight than explosives, but lower than 3460: 2912:{\displaystyle \Delta v\ =v_{e}\ln {\frac {m_{0}}{m_{1}}}} 2167:
varies based on external air pressure. From top to bottom:
2092:, permitting a weaker, and hence lighter, launch vehicle. 558:
Robert Goddard with a liquid oxygen-gasoline rocket (1926)
337:
Medieval and early modern rockets were used militarily as
292:
by the 13th century. They also developed an early form of
8273: 6856:
Coplanar Air Launch with Gravity-Turn Launch Trajectories
5407:
Developments of Rocketry and Space Technology in the USSR
1993: 1492: 1472: 1194:
chamber, and the resultant hot gases accelerate out of a
5803: 4546: – Collection of matter whose mass varies with time 2016:
Flying rockets are primarily affected by the following:
1703:
and a rocket car holds the all time (albeit unofficial)
570:
published proposed improvements to rocket technology in
7718: 6386:. Colorado Space News. 4 September 2014. Archived from 5647:"Rocket bicycle sets 207mph speed record By Leo Kelion" 4630:
Pages displaying short descriptions of redirect targets
7723: 7713: 6384:"CSXT Go Fast! Rocket Confirms Multiple World Records" 5754:, Washington (DC): John Wiley & Sons, loc 58-13458 4540: – Location used to launch and receive spacecraft 1614:
A successful escape of a crewed capsule occurred when
7734:
Asoc. Coheteria Experimental y Modelista de Argentina
5704:. Annapolis, MD: Naval Institute Press. p. 581. 4935:"Rockets in Ancient Times (100 B.C. to 17th Century)" 4671: – Test platform pushed by rockets along a track 4418: 4188: 4125: 4080: 4058: 3976: 3954: 3934: 3907: 3865: 3805: 3669: 3545: 3499: 3477: 3167:
to force the propellant into the combustion chamber.
3068: 3017: 2988: 2959: 2930: 2856: 2822: 2755: 2725: 2693: 2633: 2601: 2433: 2394: 2335: 2297: 2262: 2202: 288:-powered rockets evolved in medieval China under the 7719:
National Aeronautics and Space Administration (NASA)
7267:. Jane's Civil Aerospace. 2003-02-03. Archived from 4997:
Throwing Fire: Projectile Technology Through History
4704:
Pages displaying wikidata descriptions as a fallback
4657:
Pages displaying wikidata descriptions as a fallback
4637: – Soviet/Russian multiple launch rocket system 4444: 4307:
torn apart T+73 seconds after hot gases escaped the
4246: 2009:. Spacecraft are further studied in the subfield of 1450:
try to stop them. Rockets have also been tested for
234:), two liquids that spontaneously react on contact ( 7646:"U.S. Rocket Supplier Looks to Break 'Short Leash'" 5102:
Journal of the Society for Army Historical Research
4253:
List of spaceflight-related accidents and incidents
1380:However, they are also useful in other situations: 767:projectile. These used solid chemical propellants. 6311:. National Association of Rocketry. Archived from 5892: 5553: 4816: 4596:Pages displaying short descriptions with no spaces 4201: 4138: 4109: 4064: 4052:And the overall (instantaneous) energy efficiency 4042: 3960: 3940: 3920: 3878: 3827: 3786: 3558: 3525: 3483: 3095: 3029: 3009:is the effective exhaust velocity in m/s (or ft/s) 3001: 2972: 2943: 2911: 2835: 2771: 2738: 2709: 2675: 2617: 2449: 2415: 2348: 2314: 2281: 2244: 1635: 1333:, differed significantly from modern rockets. The 763:in the artillery role, and the American anti tank 246:), or solid fuel with liquid or gaseous oxidizer ( 230:that disassociates in the presence of a catalyst ( 7693:the government's monopoly on space travel is over 5599:"V2: The Nazi rocket that launched the space age" 4711: – Traditional festival of Laos and Thailand 8654: 7751:IMR – German/Austrian/Swiss Rocketry Association 7572: 7570: 7568: 7566: 6809: 6645:"Launch Pad Vibroacoustics Research at NASA/KSC" 5590: 5538:Ordway, Frederick I., III.; Sharpe, Mitchell R. 1573:those on board. Rockets are also used to launch 1202:) at the rearward-facing end of the rocket. The 770:The Americans captured a large number of German 7497:"Space Shuttle and International Space Station" 6946: 6944: 6942: 6940: 5444: 5442: 5160:, University of Chicago Press, pp. 46–62, 4932: 4381:, expenses of $ 2000–$ 10,000+ per kilogram of 2746:is the acceleration at the surface of the Earth 1988: 757:list of World War II guided missiles of Germany 505:(6 rockets at a time), and gun-laying devices. 474:was a British weapon designed and developed by 345:. Between 1270 and 1280, Hasan al-Rammah wrote 6272: 5749: 1174:engines or simple pressurized rockets such as 649:of aircraft and became the prototypes for the 513:further improved the Congreve rocket in 1865. 445:(part of present-day India) under the rule of 242:), a solid combination of fuel with oxidizer ( 7830: 7714:FAA Office of Commercial Space Transportation 7668: 7563: 7441:"Space Shuttle Use of Propellants and Fluids" 7242:. Astronautix.com. 2006-11-08. Archived from 6608: 6342:National Aeronautics and Space Administration 6026:"Spaceflight Now – worldwide launch schedule" 5251:"The Rockets That Inspired Francis Scott Key" 4893: 4522: – Non-functional rocket or rocket stage 3654:Energy from the fuel is lost in air drag and 3539:is the instantaneous mass of the vehicle and 2802:'s around the Solar System between Earth and 2044:; usually relatively small effect except for 1304:For smaller, low performance rockets such as 674:, and also pioneered the concept of a rocket 7637: 7591:"Europe to press ahead with Ariane 6 rocket" 7582: 6937: 5439: 5414: 5221:"rocket and missile system | weapons system" 4717: – Mail delivery by rockets or missiles 3471:From Newton's second law, the acceleration, 3320:13,000 kg (~28,660 lb) (12.8 ton) 2783: 2425:When there is fixed thrust, this is simply: 1520:Larger rockets are normally launched from a 1410:Some military weapons use rockets to propel 849:) culminated in 1969 with the first crewed 743:, either for assisting horizontal take-off ( 312:at a feast held in her honor by her son the 7607: 7332: 7202: 6514:"Rocket men's quest for command of the Ayr" 6257:. Science.howstuffworks.com. Archived from 6230:. Encyclopedia Astronautica. Archived from 6142:. Encyclopedia Astronautica. Archived from 6111:. Encyclopedia Astronautica. Archived from 5926:History of Liquid Propellant Rocket Engines 5890: 5674: 4318:Because of the enormous chemical energy in 2066:These forces, with a stabilizing tail (the 1146:. A rocket engine can use gas propellants, 371:described rockets in his military treatise 129:. To control their flight, rockets rely on 7837: 7823: 7421:"A Rocket a Day Keeps the High Costs Away" 7107: 7105: 7066:. Exploration.grc.nasa.gov. Archived from 6604: 6602: 6600: 5679:. Washington, DC: Brassey's. p. 304. 5675:Polmar, Norman; Moore, Kenneth J. (2004). 5596: 5343: 5341: 5072:History of Science and Technology in Islam 5038:History of Science and Technology in Islam 4894:Sutton, George P.; Biblarz, Oscar (2001). 4810: 4808: 4643: – Shoulder-launched anti-tank weapon 4311:, causing the breakup of the Shuttle stack 3589:vehicles employ or have employed rockets. 2446: 2228: 1812:exponentially increasing fuel requirements 1311: 27:Vehicle propelled by a reaction gas engine 7674: 7340:"Weighing the risks of human spaceflight" 7128: 7126: 7086: 7084: 6815: 6073: 6071: 5131:. Westport: Greenwood Press. p. 10. 4557:Ammonium perchlorate composite propellant 4502:Timeline of rocket and missile technology 2368:due to the reduction in propellant load. 2311: 2278: 1830:When launching a spacecraft to orbit, a " 715:began in Germany. It was designed by the 266:Timeline of rocket and missile technology 7803:Robert Goddard – America's Space Pioneer 7613: 7416: 7414: 7412: 7410: 6950: 6852: 5597:Hollingham, Richard (8 September 2014). 5297: 5022: 4926: 4823:. University of Missouri Press. p.  4814: 4291: 4119:For example, from the equation, with an 4110:{\displaystyle \eta =\eta _{p}\eta _{c}} 3892: 3622: 3407: 3399: 3120: 2793: 2245:{\displaystyle F_{n}={\dot {m}}\;v_{e},} 2159: 2122:Drag can be minimised by an aerodynamic 1992: 1949: 1913: 1851: 1817: 1717: 1548: 1471: 1397: 1315: 1223: 1114: 869: 790:, the first crewed vehicle to break the 695: 670:was released. It showcased the use of a 616: 553: 451: 421: 269: 40: 8322:Effect of spaceflight on the human body 7643: 7102: 6868: 6866: 6597: 5899:. Twenty-First Century Books. pp.  5895:Rocket man: the story of Robert Goddard 5551: 5403: 5397: 5371: 5347: 5338: 5151: 4889: 4887: 4885: 4883: 4881: 4879: 4877: 4875: 4873: 4871: 4805: 4609: – U.S. model rocketry association 3651:of the body of the rocket as possible. 3461:Acceleration and thrust-to-weight ratio 3262:2,040,000 kg (~4,500,000 lb) 3242:3,038,500 kg (~6,700,000 lb) 2676:{\displaystyle v_{e}=I_{sp}\cdot g_{0}} 1867:exhaust collides with the ambient air, 1502:Rocket engines are also used to propel 1461: 1156:hybrid mixture of both solid and liquid 1126:Rocket engines employ the principle of 1018:, a place to put propellant (such as a 786:, and further techniques; note too the 347:al-furusiyyah wa al-manasib al-harbiyya 14: 8655: 8344:Psychological and sociological effects 7173: 7171: 7169: 7167: 7165: 7123: 7081: 6897:. Geae.com. 2012-09-07. Archived from 6846: 6759: 6701: 6511: 6505: 6412:. U.S. National Archives. June 7, 1961 6252: 6164: 6068: 5965: 5923: 5917: 5644: 5542:. Apogee Books Space Series 36. p. 38. 5410:. Novosti Press Pub. House. p. 7. 5354:A Method of Reaching Extreme Altitudes 5335:, "'The First Guided Missile' p. 436 5314: 5248: 5166:10.7208/chicago/9780226720838.003.0003 5095: 4994: 4869: 4867: 4865: 4863: 4861: 4859: 4857: 4855: 4853: 4851: 4655: – Soviet supercavitating torpedo 4353: 3203:746,000 kg (~1,645,000 lb) 3096:{\displaystyle {\frac {m_{0}}{m_{1}}}} 573:A Method of Reaching Extreme Altitudes 7818: 7777:Rocket and Missile Alphabetical Index 7724:National Association of Rocketry (US) 7472:"NASA Launch Vehicles and Facilities" 7407: 7257: 6834:from the original on 19 November 2017 6733: 6367:"Organizational statement of the NAR" 5560:. New York: The Free Press. pp.  5464: 5126: 3441:This problem is frequently solved by 2980:is the final total mass in kg (or lb) 829:) and in the United States (e.g. the 739:programme, rockets were also used on 7588: 7265:"A brief history of space accidents" 7208: 7041:. Istp.gsfc.nasa.gov. Archived from 6863: 6168:Soviet and Russian lunar exploration 6028:. Spaceflightnow.com. Archived from 5808:. Concise Britannica. Archived from 5700:III, compiled by A.D. Baker (2000). 5578:from the original on 28 October 2019 4914:from the original on 12 January 2014 4628: – Chinese gunpowder projectile 4256: 3855:rearward. This phenomenon is termed 3612: 3526:{\displaystyle a={\frac {F_{n}}{m}}} 3357:~181,000 kg (400,000 lb ) 3133:Rockets as a group have the highest 2053:inertia and centrifugal pseudo-force 2005:on a rocket is part of the field of 690:The Rocket into Interplanetary Space 637:research and development laboratory 407:, an important early modern work on 363:of 1267. Between 1280 and 1300, the 332:'fire-dragon issuing from the water' 308:, had frightened the Empress-Mother 7746:United Kingdom Rocketry Association 7675:Davenport, Christian (2016-08-19). 7430:by John Walker. September 27, 1993. 7162: 6822:. D. Van Nostrand Co. p. 209. 6512:Taylor, Marianne (27 August 2007). 6372:. National Association of Rocketry. 6001:"Test sets world land speed record" 5959: 5938: 5699: 4848: 4603: – U.S. nonprofit organization 3796:100% efficiency within the engine ( 3375:~363,000 kg (800,000 lb) 3301:10,024.39 kg (22,100 lb) 2462: 1440:intercontinental ballistic missiles 1066:, which usually holds the payload. 1032:directional stabilization device(s) 815:intercontinental ballistic missiles 482:. It was Congreve rockets to which 405:Artis Magnae Artilleriae pars prima 24: 8053:Weather and environment monitoring 7761:Indian Space Research Organisation 7589:Amos, Jonathan (3 December 2014). 6794:. NASA. 2000-09-19. Archived from 6609:Potter, R.C; Crocker, M.J (1966), 6434:. Eurodragster.com. Archived from 5975:Johns Hopkins APL Technical Digest 5274: 5062: 5028: 4528: – Outdoor museum of rocketry 4419:2010s emerging private competition 3822: 3415:while dropping the interstage ring 3282:448,648 kg (989,100 lb) 3223:117,020 kg (258,000 lb) 3018: 2857: 853:– using equipment launched by the 625:fires at German forces during the 25: 8699: 7788:Complete Rocket and Missile Lists 7702: 6971:"table of cislunar/mars delta-vs" 6853:Callaway, David W. (March 2004). 6485:"Rocket blasts into record books" 6457:"'Amateur' rocket launch delayed" 6171:. Berlin: Springer. p. 226. 6081:. Astronautix.com. Archived from 5752:Fundamentals of Advanced Missiles 4247:Safety, reliability and accidents 2126:and by using a shape with a high 1580:Some crewed rockets, notably the 1434:if it is unguided. Anti-tank and 1026:. They may also have one or more 388:The name "rocket" comes from the 8636: 8626: 8625: 7756:Canadian Association of Rocketry 7614:Belfiore, Michael (2013-12-09). 7539: 7514: 7489: 7464: 7433: 6819:Sourcebook on the Space Sciences 6732:The confusion is illustrated in 6284:National Association of Rocketry 6221: 6203:from the original on 17 May 2015 6133: 6105:"N1 Manned Lunar Launch Vehicle" 6102: 6051:"Apollo launch escape subsystem" 5947:from the original on 2 June 2016 5301:The Details of the Rocket System 5249:Winter, Frank (September 2014). 4649: – Korean fire arrow rocket 4601:National Association of Rocketry 4475: 4461: 4447: 4260: 4216: 3338:15,420 kg (34,000 lb) 3304:1,678.3 kg (3,700 lb) 3285:41,594 kg (91,700 lb) 2371: 1655:National Association of Rocketry 1489:first images of Earth from space 1442:can be used to deliver multiple 1259:burned with an oxidizer such as 1138:, but some employ a decomposing 751:"Natter") or for powering them ( 583:Die Rakete zu den Planetenräumen 535:designed a guided rocket during 151:deflection of the exhaust stream 8097:Space launch market competition 7844: 7663:Launch's chief executive, said. 7503:from the original on 2011-05-07 7362: 7321:from the original on 2011-01-07 7307: 7296:from the original on 2012-09-11 7282: 7232: 7144: 7056: 7031: 7020:from the original on 2010-05-29 7006: 6995:from the original on 2000-03-12 6981: 6963: 6912: 6887: 6792:"Four forces on a model rocket" 6784: 6753: 6726: 6695: 6669: 6637: 6633:from the original on 2013-12-06 6565: 6536: 6477: 6449: 6424: 6402: 6376: 6359: 6326: 6301: 6255:"Howstuff works ejection seats" 6246: 6215: 6185: 6158: 6127: 6096: 6057:from the original on 2012-07-16 6043: 6018: 5993: 5932: 5884: 5849: 5823: 5797: 5758: 5743: 5728:. The Rocketman. Archived from 5718: 5693: 5668: 5657:from the original on 2014-11-11 5638: 5621:"NASA History: Rocket vehicles" 5613: 5545: 5532: 5507: 5482: 5458: 5377: 5325: 5308: 5291: 5268: 5242: 5231:from the original on 2017-10-31 5213: 5187: 5145: 5120: 5089: 5019:Needham, Volume 5, Part 7, 510. 4790: 4787:) ... in a gravity-free vacuum" 4757: 4748: 4559: – Solid-rocket propellant 3828:{\displaystyle \eta _{c}=100\%} 3341:6,620 kg (14,600 lb) 3226:4,760 kg (10,500 lb) 3037:is the delta-v in m/s (or ft/s) 2329:The effective exhaust velocity 2155:Rocket engine § Net thrust 1653:According to the United States 1636:Hobby, sport, and entertainment 1085:). Vehicles frequently possess 1081:), even, in a sense, a person ( 794:(1947). Independently, in the 717:Peenemünde Army Research Center 664:'s German science fiction film 588:The Rocket into Planetary Space 8334:Health threat from cosmic rays 7346:. 21 July 2003. Archived from 7290:"Rogers commission Appendix F" 7016:. Projectrho.com. 2012-06-01. 6734:Brain, Marshall (April 2000). 5804:Charles Lafayette Proctor II. 5127:Riper, A. Bowdoin Van (2004). 5056: 4988: 4956: 4729: 4028: 4014: 3110: 2289:propellant flow (kg/s or lb/s) 2194:The net thrust of a rocket is 1699:, and have been used to power 1509: 499:Alexander Dmitrievich Zasyadko 274:Rocket arrows depicted in the 91:without using any surrounding 13: 1: 7793:Rocketdyne Technical Articles 6957:Rocket & Space Technology 5806:"internal combustion engines" 5623:. Hq.nasa.gov. Archived from 5465:Weide, Robert (Summer 2012). 4964:"A brief history of rocketry" 4516: – Branch of engineering 3928:for a rocket moving at speed 2482:in vacuum of various rockets 2282:{\displaystyle {\dot {m}}=\,} 2148: 2084:, which minimizes transverse 1446:from thousands of miles, and 1213: 1054:) and a structure (typically 1009: 981:rapid escape systems such as 833:). Rockets came into use for 798:research continued under the 79:'bobbin/spool') is a 7729:Tripoli Rocketry Association 7644:Pasztor, Andy (2015-09-17). 6951:Braeunig, Robert A. (2008). 6922:. Thrust SSC. Archived from 6253:Bonsor, Kevin (2001-06-27). 6003:. www.af.mil. Archived from 5941:"What is a Sounding Rocket?" 5891:Streissguth, Thomas (1995). 5552:Neufeld, Michael J. (1995). 5449:"The Directors (Fritz Lang)" 5199:. Milano: Arcadia Edizioni. 4939:A Timeline of Rocket History 4607:Tripoli Rocketry Association 3837:high expansion ratio nozzles 1997:Forces on a rocket in flight 1989:Forces on a rocket in flight 1903: 1685:: low-power, mid-power, and 837:. American crewed programs ( 796:Soviet Union's space program 727:with the vertical launch of 598:) nozzle to a high pressure 7: 8450:Self-replicating spacecraft 8286:International Space Station 7782:Rocket and Space Technology 7579:. Retrieved April 29, 2011. 7215:Beginner's Guide to Rockets 6708:. London: Murray. pp.  6573:"Another task for the PSLV" 6136:"N1 5L launch – 1969.07.03" 5862:The Pendulum Rocket Fallacy 5455:. Season 1, episode 6. 2018 5298:Congreve, William (2018) . 5277:"MLRS and Maneuver Warfare" 4440: 4429:Since the early 2010s, new 3297:Virgin Atlantic GlobalFlyer 2845:Tsiolkovsky rocket equation 2790:Tsiolkovsky rocket equation 1808:vehicles have been proposed 1595:This was the case when the 1383: 1136:internal combustion engines 1099:inertial navigation systems 918:that can be purchased at a 176:. Rockets are now used for 10: 8704: 7964:Space Liability Convention 7039:"The Evolution of Rockets" 6876:. Aerospaceweb. 2001-05-06 6816:Glasstone, Samuel (1965). 6766:. London: Murray. p.  6677:"Sound Suppression System" 6618:, Washington, D.C.: NASA, 6280:"Model Rocket Safety Code" 5924:Sutton, George P. (2006). 5645:Kelion, Leo (2013-11-11). 5404:Glushko, Valentin (1973). 5331:'Flight 3 October 1952, 5318:God's Glory in the Heavens 5279:. Marine Corps Association 4995:Crosby, Alfred W. (2002). 4897:Rocket Propulsion Elements 4702: – strategy card game 4437:into the existing market. 4422: 4250: 4220: 3616: 3602:gravitational acceleration 3491:, of a vehicle is simply: 3464: 3393: 3389: 3114: 3030:{\displaystyle \Delta v\ } 2787: 2466: 2416:{\displaystyle I=\int Fdt} 2375: 2324:effective exhaust velocity 2152: 2099: 1907: 1898: 1695:rockets are used to power 1639: 1513: 1465: 1387: 1306:attitude control thrusters 1217: 1162:of propellant(s), such as 1108: 1104: 711:In 1943 production of the 522:God's Glory in the Heavens 263: 257: 253: 139:auxiliary reaction engines 31: 8620: 8587: 8540: 8492: 8378: 8327:Space adaptation syndrome 8314: 8219: 8139: 8130: 8018: 7852: 7773:Encyclopedia Astronautica 7383:10.1109/RAMS.2006.1677430 7317:. Space.com. 2004-09-30. 7240:"Astronautix NK-33 entry" 7134:"Astronautix – Saturn IB" 7092:"Astronautix – Ariane 5g" 6736:"How Rocket Engines Work" 5380:"Gas Dynamics Laboratory" 5152:Grafton, Anthony (2007), 4900:. John Wiley & Sons. 4202:{\displaystyle \eta _{c}} 4182:—in spite of their worse 4139:{\displaystyle \eta _{c}} 3948:with an exhaust velocity 3921:{\displaystyle \eta _{p}} 3879:{\displaystyle \eta _{p}} 3607: 2784:Delta-v (rocket equation) 2001:The general study of the 1975:). From the principle of 1713: 1544: 1353:Rockets or other similar 997: 653:, which were used during 623:Katyusha rocket launchers 461:bombardment of Copenhagen 240:liquid-propellant rockets 117:are capable of attaining 8060:Communications satellite 7113:"Astronautix – Saturn V" 6338:exploration.grc.nasa.gov 5966:Fraser, Lorence (1985). 5315:Leitch, William (1862). 5255:Air & Space Magazine 5154:"The Devil as Automaton" 4763:"thrust-to-weight ratio 4722: 4641:Rocket-propelled grenade 4635:Katyusha rocket launcher 4615: – Type of firework 4413:rocket-assisted take off 3103:is sometimes called the 2315:{\displaystyle v_{e}=\,} 1977:conservation of momentum 1847: 860: 651:Katyusha rocket launcher 643:solid-propellant rockets 415:, was first printed in 294:multiple rocket launcher 248:hybrid propellant system 174:setting foot on the Moon 8678:Rocket-powered aircraft 8564:reusable launch systems 8181:Extravehicular activity 8092:Commercial use of space 7996:Militarisation of space 7969:Registration Convention 7885:Accidents and incidents 7651:The Wall Street Journal 5750:Richard B. Dow (1958), 5225:Encyclopædia Britannica 4338:, having served on the 3153:orbital launch vehicles 2095: 2046:rocket-powered aircraft 2038:if moving in atmosphere 1730:Video of the launch of 1650:by a variety of means. 1628:Solid rocket propelled 1625:, exploded on the pad. 1597:Safety Assurance System 1448:anti-ballistic missiles 1348: 1312:Pendulum rocket fallacy 1299:nuclear thermal rockets 1286:decomposed to hot gas. 951:rocket-powered aircraft 639:Gas Dynamics Laboratory 543:stated "...in 1917 the 34:Rocket (disambiguation) 8612:Mission control center 8574:Non-rocket spacelaunch 8008:Billionaire space race 7786:Gunter's Space Page – 7474:. NASA. Archived from 7446:. NASA. Archived from 7217:. NASA. Archived from 6895:"General Electric J85" 6760:Warren, J. W. (1979). 6702:Warren, J. W. (1979). 6165:Harvey, Brian (2007). 5838:. NASA. Archived from 5096:McCaig, A. D. (2000). 4941:. NASA. Archived from 4815:Bernhard, Jim (2007). 4700:Launch Pad (card game) 4580:Nuclear thermal rocket 4403:non-rocket spacelaunch 4312: 4203: 4140: 4111: 4066: 4044: 3962: 3942: 3922: 3898: 3880: 3829: 3788: 3639: 3579:thrust-to-weight ratio 3560: 3527: 3485: 3467:thrust-to-weight ratio 3423:, tankage, structure, 3416: 3405: 3135:thrust-to-weight ratio 3126: 3097: 3031: 3003: 2974: 2945: 2913: 2837: 2806: 2773: 2772:{\displaystyle I_{sp}} 2740: 2711: 2710:{\displaystyle I_{sp}} 2677: 2619: 2618:{\displaystyle I_{sp}} 2451: 2450:{\displaystyle I=Ft\;} 2417: 2357:within an atmosphere. 2350: 2316: 2283: 2246: 2189:thrust-to-weight ratio 2184: 1998: 1955: 1941:conservation of energy 1919: 1860: 1827: 1766:mission control center 1762:firing control systems 1746: 1618:, on a mission to the 1562: 1481: 1436:anti-aircraft missiles 1420:when the weapon has a 1407: 1322: 1229: 1172:nuclear thermal rocket 1123: 895: 866:Vehicle configurations 802:of the chief designer 747:), vertical take-off ( 733:Science Museum, London 708: 630: 580:(1894–1989) published 559: 526:Konstantin Tsiolkovsky 467: 434: 281: 236:hypergolic propellants 69: 57: 49:rocket launches from " 8688:Space launch vehicles 8462:Spacecraft propulsion 7912:European Space Agency 7119:on February 28, 2002. 7098:on December 25, 2003. 6874:"Space Shuttle Max-Q" 6199:. 2015 YouTube, LLC. 5832:Discover NASA and You 4933:MSFC History Office. 4694:Equivalence principle 4586:Recreational rocketry 4520:Battleship (rocketry) 4514:Aerospace engineering 4423:Further information: 4334:, American physicist 4295: 4204: 4141: 4112: 4067: 4065:{\displaystyle \eta } 4045: 3963: 3943: 3923: 3896: 3881: 3857:propulsive efficiency 3830: 3789: 3626: 3619:propulsive efficiency 3561: 3559:{\displaystyle F_{n}} 3528: 3486: 3429:Single-stage-to-orbit 3411: 3403: 3124: 3098: 3032: 3004: 3002:{\displaystyle v_{e}} 2975: 2973:{\displaystyle m_{1}} 2946: 2944:{\displaystyle m_{0}} 2914: 2838: 2836:{\displaystyle v_{e}} 2798:A map of approximate 2797: 2774: 2741: 2739:{\displaystyle g_{0}} 2712: 2678: 2620: 2452: 2418: 2351: 2349:{\displaystyle v_{e}} 2317: 2284: 2247: 2163: 2128:ballistic coefficient 1996: 1953: 1937:Bernoulli's principle 1917: 1855: 1821: 1802:All current vehicles 1729: 1590:launch escape systems 1552: 1527:artificial satellites 1491:were obtained from a 1475: 1401: 1319: 1227: 1168:solar thermal rockets 1118: 1014:Rockets consist of a 987:launch escape systems 932:such as the enormous 878: 699: 620: 557: 455: 425: 273: 264:Further information: 198:artificial satellites 44: 8663:Rockets and missiles 8087:Satellite navigation 7377:. pp. 545–550. 7179:"AIAA2001-4619 RLVs" 7064:"Rocket Mass Ratios" 7014:"Choose Your Engine" 6953:"Rocket Propellants" 6524:on 30 September 2007 5767:"4. Rocket Vehicles" 5304:. Project Gutenberg. 5044:on February 26, 2008 4663:Rockets for research 4574:Tripropellant rocket 4544:Variable-mass system 4370:, 60% solids in the 4186: 4123: 4078: 4056: 3974: 3952: 3932: 3905: 3863: 3803: 3667: 3543: 3497: 3475: 3259:(vehicle + payload) 3200:(vehicle + payload) 3066: 3015: 2986: 2957: 2928: 2854: 2820: 2753: 2723: 2717:has units of seconds 2691: 2631: 2599: 2431: 2392: 2333: 2295: 2260: 2200: 2180:Grossly overexpanded 2145:under these forces. 2134:as low as possible. 2076:trajectory termed a 1755:interplanetary space 1751:orbital spaceflights 1462:Science and research 1295:solar thermal rocket 1196:rocket engine nozzle 1095:satellite navigation 902:tiny models such as 647:jet-assisted takeoff 627:Battle of Stalingrad 621:A battery of Soviet 511:Edward Mounier Boxer 476:Sir William Congreve 413:Casimir Siemienowicz 397:Leonhard Fronsperger 123:airbreathing engines 32:For other uses, see 8472:Electric propulsion 8159:Life-support system 8043:Imagery and mapping 8003:Private spaceflight 7453:on October 17, 2011 7350:on 23 November 2010 6989:"cislunar delta-vs" 6115:on 21 February 2012 5275:Morris, Charles W. 5227:(Online ed.). 4592:High-power rocketry 4563:Pulsed rocket motor 4354:Costs and economics 4239:it gains or loses. 3722: 3638:during launch phase 2483: 1228:Gas Core light bulb 1093:that typically use 916:small solid rockets 851:landing on the Moon 776:Operation Paperclip 562:In 1920, Professor 153:, propellant flow, 99:produces thrust by 55:Baikonur Cosmodrome 8668:Chinese inventions 8425:Robotic spacecraft 8351:Space and survival 8206:Space colonization 8102:Space architecture 7954:Outer Space Treaty 7808:2009-02-05 at the 7739:2020-10-27 at the 7708:Governing agencies 7545:Regis, Ed (1990), 7426:2008-11-03 at the 5467:"The Outer Limits" 4483:Spaceflight portal 4368:external fuel tank 4320:rocket propellants 4313: 4272:. You can help by 4199: 4136: 4107: 4062: 4040: 3958: 3938: 3918: 3899: 3876: 3825: 3784: 3708: 3640: 3556: 3523: 3481: 3417: 3406: 3127: 3093: 3027: 2999: 2970: 2941: 2909: 2833: 2807: 2769: 2736: 2707: 2673: 2615: 2473: 2447: 2413: 2346: 2312: 2279: 2242: 2185: 2165:A rocket jet shape 2023:from the engine(s) 1999: 1973:Newton's Third Law 1956: 1945:Newton's third law 1929:combustion chamber 1920: 1861: 1828: 1747: 1563: 1482: 1408: 1404:Trident II missile 1327:liquid-fuel rocket 1323: 1321:vehicle to rotate. 1230: 1208:Newton's Third Law 1180:cold gas thrusters 1142:) that emit a hot 1124: 1087:navigation systems 1062:fairing such as a 896: 709: 672:multi-stage rocket 631: 608:liquid propellants 600:combustion chamber 560: 545:Experimental Works 533:Royal Flying Corps 468: 463:(1807) during the 435: 339:incendiary weapons 282: 260:History of rockets 115:Multistage rockets 58: 8650: 8649: 8597:Flight controller 8374: 8373: 8132:Human spaceflight 8107:Space exploration 8033:Earth observation 7767:Information sites 7158:on March 2, 2002. 7152:"Astronautix-V-2" 7140:on March 5, 2002. 6777:978-0-7195-3564-2 6740:Howstuffworks.com 6719:978-0-7195-3564-2 6544:"Moonport, CH1-2" 6178:978-0-387-73976-2 5939:Marconi, Elaine. 5869:). Archived from 5711:978-1-55750-197-4 5686:978-1-57488-594-1 5477:Woman in the Moon 5384:Russian Space Web 5206:978-88-85684-06-5 5175:978-0-226-72081-4 5138:978-0-313-32795-7 5006:978-0-521-79158-8 4907:978-0-471-32642-7 4834:978-0-8262-6601-9 4551:Rocket propulsion 4532:Service structure 4340:Rogers Commission 4290: 4289: 4038: 4025: 4004: 3961:{\displaystyle c} 3941:{\displaystyle u} 3849:jet-based engines 3842:Carnot efficiency 3798:engine efficiency 3782: 3705: 3694: 3613:Energy efficiency 3521: 3484:{\displaystyle a} 3396:Multistage rocket 3387: 3386: 3091: 3026: 2907: 2865: 2586: 2585: 2378:Impulse (physics) 2272: 2225: 2051:In addition, the 1778:tracking stations 1727: 1693:Hydrogen peroxide 1406:launched from sea 1331:Robert H. Goddard 1329:, constructed by 1280:hydrogen peroxide 1240:in the form of a 1220:Rocket propellant 1160:chemical reaction 1152:liquid propellant 876: 835:space exploration 772:rocket scientists 721:Wernher von Braun 667:Woman in the Moon 641:began developing 484:Francis Scott Key 443:Kingdom of Mysore 328:multistage rocket 302:military exercise 206:space exploration 202:human spaceflight 78: 16:(Redirected from 8695: 8640: 8629: 8628: 8339:Space psychology 8164:Animals in space 8137: 8136: 8117:Space technology 7959:Rescue Agreement 7839: 7832: 7825: 7816: 7815: 7696: 7695: 7690: 7689: 7672: 7666: 7665: 7659: 7658: 7641: 7635: 7634: 7632: 7631: 7622:. Archived from 7611: 7605: 7604: 7602: 7601: 7586: 7580: 7574: 7561: 7543: 7537: 7536: 7534: 7533: 7518: 7512: 7511: 7509: 7508: 7493: 7487: 7486: 7484: 7483: 7468: 7462: 7461: 7459: 7458: 7452: 7445: 7437: 7431: 7418: 7405: 7404: 7366: 7360: 7359: 7357: 7355: 7344:The Space Review 7336: 7330: 7329: 7327: 7326: 7311: 7305: 7304: 7302: 7301: 7286: 7280: 7279: 7277: 7276: 7261: 7255: 7254: 7252: 7251: 7236: 7230: 7229: 7227: 7226: 7211:"Rocket staging" 7206: 7200: 7199: 7197: 7196: 7190: 7184:. Archived from 7183: 7175: 7160: 7159: 7154:. Archived from 7148: 7142: 7141: 7136:. Archived from 7130: 7121: 7120: 7115:. Archived from 7109: 7100: 7099: 7094:. Archived from 7088: 7079: 7078: 7076: 7075: 7060: 7054: 7053: 7051: 7050: 7035: 7029: 7028: 7026: 7025: 7010: 7004: 7003: 7001: 7000: 6985: 6979: 6978: 6973:. Archived from 6967: 6961: 6960: 6948: 6935: 6934: 6932: 6931: 6916: 6910: 6909: 6907: 6906: 6891: 6885: 6884: 6882: 6881: 6870: 6861: 6860: 6850: 6844: 6843: 6841: 6839: 6813: 6807: 6806: 6804: 6803: 6788: 6782: 6781: 6757: 6751: 6750: 6748: 6746: 6730: 6724: 6723: 6699: 6693: 6692: 6690: 6688: 6679:. Archived from 6673: 6667: 6666: 6664: 6662: 6656: 6650:. Archived from 6649: 6641: 6635: 6634: 6632: 6617: 6606: 6595: 6594: 6592: 6591: 6569: 6563: 6562: 6560: 6559: 6550:. Archived from 6540: 6534: 6533: 6531: 6529: 6520:. Archived from 6509: 6503: 6502: 6500: 6498: 6493:. 27 August 2007 6481: 6475: 6474: 6472: 6470: 6465:. 25 August 2007 6453: 6447: 6446: 6444: 6443: 6428: 6422: 6421: 6419: 6417: 6406: 6400: 6399: 6397: 6395: 6380: 6374: 6373: 6371: 6363: 6357: 6356: 6354: 6353: 6344:. Archived from 6330: 6324: 6323: 6321: 6320: 6305: 6299: 6298: 6296: 6295: 6286:. Archived from 6276: 6270: 6269: 6267: 6266: 6250: 6244: 6243: 6241: 6239: 6234:on 5 August 2014 6219: 6213: 6212: 6210: 6208: 6189: 6183: 6182: 6162: 6156: 6155: 6153: 6151: 6131: 6125: 6124: 6122: 6120: 6100: 6094: 6093: 6091: 6090: 6075: 6066: 6065: 6063: 6062: 6053:. ApolloSaturn. 6047: 6041: 6040: 6038: 6037: 6022: 6016: 6015: 6013: 6012: 5997: 5991: 5990: 5988: 5986: 5972: 5963: 5957: 5956: 5954: 5952: 5936: 5930: 5929: 5921: 5915: 5914: 5898: 5888: 5882: 5881: 5879: 5878: 5853: 5847: 5846: 5844: 5837: 5827: 5821: 5820: 5818: 5817: 5801: 5795: 5794: 5793: 5792: 5783:, archived from 5762: 5756: 5755: 5747: 5741: 5740: 5738: 5737: 5722: 5716: 5715: 5697: 5691: 5690: 5672: 5666: 5665: 5663: 5662: 5642: 5636: 5635: 5633: 5632: 5617: 5611: 5610: 5608: 5606: 5594: 5588: 5587: 5585: 5583: 5564:, 160–162, 190. 5559: 5549: 5543: 5536: 5530: 5529: 5527: 5525: 5511: 5505: 5504: 5502: 5500: 5486: 5480: 5474: 5462: 5456: 5446: 5437: 5436: 5434: 5432: 5418: 5412: 5411: 5401: 5395: 5394: 5392: 5390: 5375: 5369: 5368: 5359: 5345: 5336: 5329: 5323: 5322: 5312: 5306: 5305: 5295: 5289: 5288: 5286: 5284: 5272: 5266: 5265: 5263: 5261: 5246: 5240: 5239: 5237: 5236: 5217: 5211: 5210: 5191: 5185: 5184: 5183: 5182: 5149: 5143: 5142: 5124: 5118: 5117: 5108:(316): 252–263. 5093: 5087: 5086: 5084: 5083: 5078:on March 9, 2008 5074:. 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Archived from 4960: 4954: 4953: 4951: 4950: 4930: 4924: 4923: 4921: 4919: 4891: 4846: 4845: 4843: 4841: 4822: 4812: 4797: 4794: 4788: 4786: 4777: 4761: 4755: 4752: 4746: 4733: 4705: 4658: 4631: 4597: 4508:General rocketry 4497:Lists of rockets 4485: 4480: 4479: 4478: 4471: 4466: 4465: 4464: 4457: 4452: 4451: 4450: 4399:reusable rockets 4300: 4285: 4282: 4264: 4257: 4208: 4206: 4205: 4200: 4198: 4197: 4145: 4143: 4142: 4137: 4135: 4134: 4116: 4114: 4113: 4108: 4106: 4105: 4096: 4095: 4071: 4069: 4068: 4063: 4049: 4047: 4046: 4041: 4039: 4037: 4036: 4035: 4026: 4018: 4006: 4005: 3997: 3991: 3986: 3985: 3967: 3965: 3964: 3959: 3947: 3945: 3944: 3939: 3927: 3925: 3924: 3919: 3917: 3916: 3885: 3883: 3882: 3877: 3875: 3874: 3834: 3832: 3831: 3826: 3815: 3814: 3793: 3791: 3790: 3785: 3783: 3781: 3780: 3779: 3761: 3760: 3723: 3721: 3716: 3707: 3706: 3698: 3695: 3687: 3684: 3679: 3678: 3649:potential energy 3631: 3598:vertical landing 3594:vertical takeoff 3565: 3563: 3562: 3557: 3555: 3554: 3538: 3532: 3530: 3529: 3524: 3522: 3517: 3516: 3507: 3490: 3488: 3487: 3482: 3173: 3172: 3102: 3100: 3099: 3094: 3092: 3090: 3089: 3080: 3079: 3070: 3057:gaining altitude 3036: 3034: 3033: 3028: 3024: 3008: 3006: 3005: 3000: 2998: 2997: 2979: 2977: 2976: 2971: 2969: 2968: 2950: 2948: 2947: 2942: 2940: 2939: 2918: 2916: 2915: 2910: 2908: 2906: 2905: 2896: 2895: 2886: 2878: 2877: 2863: 2842: 2840: 2839: 2834: 2832: 2831: 2778: 2776: 2775: 2770: 2768: 2767: 2745: 2743: 2742: 2737: 2735: 2734: 2716: 2714: 2713: 2708: 2706: 2705: 2682: 2680: 2679: 2674: 2672: 2671: 2659: 2658: 2643: 2642: 2624: 2622: 2621: 2616: 2614: 2613: 2593:specific Impulse 2484: 2472: 2469:specific impulse 2463:Specific impulse 2456: 2454: 2453: 2448: 2422: 2420: 2419: 2414: 2355: 2353: 2352: 2347: 2345: 2344: 2321: 2319: 2318: 2313: 2307: 2306: 2288: 2286: 2285: 2280: 2274: 2273: 2265: 2251: 2249: 2248: 2243: 2238: 2237: 2227: 2226: 2218: 2212: 2211: 2174:Ideally expanded 2110:Aerodynamic drag 2031:celestial bodies 1982:specific impulse 1871:are formed. The 1835: 1834: 1825: 1735: 1728: 1575:emergency flares 1495:rocket in 1946 ( 1485:Sounding rockets 1456:Ping-Pong rocket 1444:nuclear warheads 1390:Rocket artillery 1355:reaction devices 1148:solid propellant 1091:guidance systems 1048:thrust vectoring 971:rocket torpedoes 877: 847:Apollo programme 707:, summer of 1943 629:, 6 October 1942 568:Clark University 457:William Congreve 439:Mysorean rockets 431:rocket artillery 427:Mysorean rockets 409:rocket artillery 379:Giovanni Fontana 298:Mongol invasions 212:Chemical rockets 143:gimballed thrust 73: 21: 8703: 8702: 8698: 8697: 8696: 8694: 8693: 8692: 8653: 8652: 8651: 8646: 8616: 8583: 8555:Escape velocity 8536: 8488: 8455:Space telescope 8408:Reentry capsule 8370: 8310: 8215: 8186:Overview effect 8169:Bioastronautics 8126: 8014: 7848: 7843: 7810:Wayback Machine 7741:Wayback Machine 7705: 7700: 7699: 7687: 7685: 7682:Washington Post 7673: 7669: 7656: 7654: 7642: 7638: 7629: 7627: 7616:"The Rocketeer" 7612: 7608: 7599: 7597: 7587: 7583: 7575: 7564: 7549:, Basic Books, 7544: 7540: 7531: 7529: 7522:"Mass Fraction" 7520: 7519: 7515: 7506: 7504: 7495: 7494: 7490: 7481: 7479: 7470: 7469: 7465: 7456: 7454: 7450: 7443: 7439: 7438: 7434: 7428:Wayback Machine 7419: 7408: 7393: 7367: 7363: 7353: 7351: 7338: 7337: 7333: 7324: 7322: 7313: 7312: 7308: 7299: 7297: 7288: 7287: 7283: 7274: 7272: 7263: 7262: 7258: 7249: 7247: 7238: 7237: 7233: 7224: 7222: 7207: 7203: 7194: 7192: 7188: 7181: 7177: 7176: 7163: 7150: 7149: 7145: 7132: 7131: 7124: 7111: 7110: 7103: 7090: 7089: 7082: 7073: 7071: 7062: 7061: 7057: 7048: 7046: 7037: 7036: 7032: 7023: 7021: 7012: 7011: 7007: 6998: 6996: 6987: 6986: 6982: 6969: 6968: 6964: 6949: 6938: 6929: 6927: 6918: 6917: 6913: 6904: 6902: 6893: 6892: 6888: 6879: 6877: 6872: 6871: 6864: 6851: 6847: 6837: 6835: 6814: 6810: 6801: 6799: 6790: 6789: 6785: 6778: 6758: 6754: 6744: 6742: 6731: 6727: 6720: 6700: 6696: 6686: 6684: 6675: 6674: 6670: 6660: 6658: 6654: 6647: 6643: 6642: 6638: 6630: 6615: 6607: 6598: 6589: 6587: 6571: 6570: 6566: 6557: 6555: 6548:www.hq.nasa.gov 6542: 6541: 6537: 6527: 6525: 6510: 6506: 6496: 6494: 6483: 6482: 6478: 6468: 6466: 6455: 6454: 6450: 6441: 6439: 6430: 6429: 6425: 6415: 6413: 6408: 6407: 6403: 6393: 6391: 6390:on 4 March 2016 6382: 6381: 6377: 6369: 6365: 6364: 6360: 6351: 6349: 6334:"Model Rockets" 6332: 6331: 6327: 6318: 6316: 6307: 6306: 6302: 6293: 6291: 6278: 6277: 6273: 6264: 6262: 6251: 6247: 6237: 6235: 6228:astronautix.com 6220: 6216: 6206: 6204: 6191: 6190: 6186: 6179: 6163: 6159: 6149: 6147: 6146:on 27 July 2015 6140:astronautix.com 6132: 6128: 6118: 6116: 6109:astronautix.com 6101: 6097: 6088: 6086: 6077: 6076: 6069: 6060: 6058: 6049: 6048: 6044: 6035: 6033: 6024: 6023: 6019: 6010: 6008: 6007:on June 1, 2013 5999: 5998: 5994: 5984: 5982: 5970: 5964: 5960: 5950: 5948: 5937: 5933: 5922: 5918: 5911: 5889: 5885: 5876: 5874: 5855: 5854: 5850: 5842: 5835: 5829: 5828: 5824: 5815: 5813: 5802: 5798: 5790: 5788: 5763: 5759: 5748: 5744: 5735: 5733: 5726:"The Rocketman" 5724: 5723: 5719: 5712: 5698: 5694: 5687: 5673: 5669: 5660: 5658: 5643: 5639: 5630: 5628: 5619: 5618: 5614: 5604: 5602: 5595: 5591: 5581: 5579: 5572: 5550: 5546: 5540:The Rocket Team 5537: 5533: 5523: 5521: 5513: 5512: 5508: 5498: 5496: 5488: 5487: 5483: 5463: 5459: 5447: 5440: 5430: 5428: 5420: 5419: 5415: 5402: 5398: 5388: 5386: 5376: 5372: 5357: 5349:Goddard, Robert 5346: 5339: 5330: 5326: 5313: 5309: 5296: 5292: 5282: 5280: 5273: 5269: 5259: 5257: 5247: 5243: 5234: 5232: 5219: 5218: 5214: 5207: 5192: 5188: 5180: 5178: 5176: 5150: 5146: 5139: 5125: 5121: 5094: 5090: 5081: 5079: 5064:Hassan, Ahmad Y 5061: 5057: 5047: 5045: 5030:Hassan, Ahmad Y 5027: 5023: 5018: 5014: 5007: 4993: 4989: 4977: 4975: 4962: 4961: 4957: 4948: 4946: 4931: 4927: 4917: 4915: 4908: 4892: 4849: 4839: 4837: 4835: 4813: 4806: 4801: 4800: 4795: 4791: 4785: 4782: 4779: 4776: 4775: 4771: 4767: 4764: 4762: 4758: 4753: 4749: 4734: 4730: 4725: 4720: 4709:Rocket Festival 4703: 4675:Sounding rocket 4656: 4629: 4595: 4481: 4476: 4474: 4469:Rocketry portal 4467: 4462: 4460: 4455:Aviation portal 4453: 4448: 4446: 4443: 4431:private options 4427: 4421: 4379:launch vehicles 4356: 4336:Richard Feynman 4296: 4286: 4280: 4277: 4270:needs expansion 4255: 4249: 4225: 4219: 4193: 4189: 4187: 4184: 4183: 4168:liquid hydrogen 4158:. For example, 4130: 4126: 4124: 4121: 4120: 4117: 4101: 4097: 4091: 4087: 4079: 4076: 4075: 4057: 4054: 4053: 4050: 4031: 4027: 4017: 4007: 3996: 3992: 3990: 3981: 3977: 3975: 3972: 3971: 3953: 3950: 3949: 3933: 3930: 3929: 3912: 3908: 3906: 3903: 3902: 3870: 3866: 3864: 3861: 3860: 3810: 3806: 3804: 3801: 3800: 3794: 3766: 3762: 3729: 3725: 3724: 3717: 3712: 3697: 3696: 3686: 3685: 3683: 3674: 3670: 3668: 3665: 3664: 3627: 3621: 3615: 3610: 3550: 3546: 3544: 3541: 3540: 3536: 3533: 3512: 3508: 3506: 3498: 3495: 3494: 3476: 3473: 3472: 3469: 3463: 3398: 3392: 3157:liquid hydrogen 3119: 3113: 3085: 3081: 3075: 3071: 3069: 3067: 3064: 3063: 3045:low Earth orbit 3038: 3016: 3013: 3012: 3010: 2993: 2989: 2987: 2984: 2983: 2981: 2964: 2960: 2958: 2955: 2954: 2952: 2935: 2931: 2929: 2926: 2925: 2901: 2897: 2891: 2887: 2885: 2873: 2869: 2855: 2852: 2851: 2827: 2823: 2821: 2818: 2817: 2792: 2786: 2760: 2756: 2754: 2751: 2750: 2747: 2730: 2726: 2724: 2721: 2720: 2718: 2698: 2694: 2692: 2689: 2688: 2683: 2667: 2663: 2651: 2647: 2638: 2634: 2632: 2629: 2628: 2606: 2602: 2600: 2597: 2596: 2568: 2547: 2530: 2519: 2506: 2498: 2480: 2471: 2465: 2457: 2432: 2429: 2428: 2423: 2393: 2390: 2389: 2380: 2374: 2340: 2336: 2334: 2331: 2330: 2327: 2302: 2298: 2296: 2293: 2292: 2290: 2264: 2263: 2261: 2258: 2257: 2252: 2233: 2229: 2217: 2216: 2207: 2203: 2201: 2198: 2197: 2183: 2158: 2151: 2132:angle of attack 2112: 2100:Main articles: 2098: 2082:angle of attack 2061:escape velocity 1991: 1912: 1906: 1901: 1873:sound intensity 1850: 1832: 1831: 1823: 1789:launch vehicles 1774:ground stations 1731: 1718: 1716: 1644: 1638: 1569:can be used to 1547: 1518: 1512: 1480:sounding rocket 1470: 1464: 1422:guidance system 1396: 1388:Main articles: 1386: 1351: 1314: 1253:liquid hydrogen 1222: 1216: 1113: 1107: 1040:vernier engines 1020:propellant tank 1012: 1000: 975:rocket-powered 904:balloon rockets 890:− 30 s through 870: 863: 839:Project Mercury 761:Katyusha rocket 480:Napoleonic Wars 472:Congreve rocket 465:Napoleonic Wars 268: 262: 256: 194:launch vehicles 147:momentum wheels 119:escape velocity 51:Gagarin's Start 37: 28: 23: 22: 15: 12: 11: 5: 8701: 8691: 8690: 8685: 8680: 8675: 8670: 8665: 8648: 8647: 8645: 8644: 8633: 8621: 8618: 8617: 8615: 8614: 8609: 8604: 8602:Ground station 8599: 8593: 8591: 8589:Ground segment 8585: 8584: 8582: 8581: 8576: 8571: 8566: 8557: 8552: 8546: 8544: 8538: 8537: 8535: 8534: 8529: 8524: 8522:Interplanetary 8519: 8518: 8517: 8515:Geosynchronous 8512: 8502: 8496: 8494: 8490: 8489: 8487: 8486: 8485: 8484: 8482:Gravity assist 8479: 8474: 8469: 8459: 8458: 8457: 8452: 8447: 8442: 8437: 8432: 8422: 8417: 8416: 8415: 8413:Service module 8410: 8405: 8403:Orbital module 8395: 8390: 8388:Launch vehicle 8384: 8382: 8376: 8375: 8372: 8371: 8369: 8368: 8366:Space sexology 8363: 8358: 8356:Space medicine 8353: 8348: 8347: 8346: 8336: 8331: 8330: 8329: 8318: 8316: 8312: 8311: 8309: 8308: 8303: 8298: 8293: 8288: 8283: 8282: 8281: 8271: 8266: 8265: 8264: 8259: 8249: 8244: 8239: 8234: 8229: 8223: 8221: 8217: 8216: 8214: 8213: 8208: 8203: 8198: 8193: 8191:Weightlessness 8188: 8183: 8178: 8177: 8176: 8171: 8166: 8156: 8155: 8154: 8143: 8141: 8134: 8128: 8127: 8125: 8124: 8119: 8114: 8112:Space research 8109: 8104: 8099: 8094: 8089: 8084: 8083: 8082: 8077: 8072: 8067: 8057: 8056: 8055: 8050: 8048:Reconnaissance 8045: 8040: 8030: 8024: 8022: 8016: 8015: 8013: 8012: 8011: 8010: 8000: 7999: 7998: 7993: 7988: 7978: 7977: 7976: 7971: 7966: 7961: 7956: 7946: 7945: 7944: 7939: 7934: 7929: 7924: 7919: 7917:European Union 7914: 7909: 7904: 7894: 7889: 7888: 7887: 7882: 7877: 7872: 7862: 7856: 7854: 7850: 7849: 7842: 7841: 7834: 7827: 7819: 7813: 7812: 7800: 7795: 7790: 7784: 7779: 7764: 7763: 7758: 7753: 7748: 7743: 7731: 7726: 7721: 7716: 7704: 7703:External links 7701: 7698: 7697: 7667: 7636: 7620:Foreign Policy 7606: 7581: 7562: 7559:Excerpt online 7538: 7513: 7488: 7463: 7432: 7406: 7391: 7361: 7331: 7306: 7281: 7256: 7231: 7201: 7161: 7143: 7122: 7101: 7080: 7055: 7030: 7005: 6991:. Strout.net. 6980: 6977:on 2007-07-01. 6962: 6936: 6911: 6886: 6862: 6845: 6808: 6783: 6776: 6752: 6725: 6718: 6694: 6668: 6636: 6596: 6579:. 2011-06-22. 6564: 6535: 6504: 6476: 6448: 6432:"Sammy Miller" 6423: 6401: 6375: 6358: 6325: 6300: 6271: 6245: 6224:"Soyuz T-10-1" 6214: 6184: 6177: 6157: 6126: 6095: 6067: 6042: 6017: 5992: 5958: 5931: 5916: 5909: 5883: 5848: 5845:on 2010-05-27. 5822: 5796: 5757: 5742: 5717: 5710: 5692: 5685: 5667: 5637: 5612: 5589: 5570: 5544: 5531: 5506: 5481: 5457: 5438: 5413: 5396: 5378:Zak, Anatoly. 5370: 5337: 5324: 5307: 5290: 5267: 5241: 5212: 5205: 5186: 5174: 5144: 5137: 5119: 5088: 5055: 5021: 5012: 5005: 4987: 4968:NASA Spacelink 4955: 4925: 4906: 4847: 4833: 4803: 4802: 4799: 4798: 4789: 4783: 4780: 4773: 4772: 4769: 4765: 4756: 4747: 4727: 4726: 4724: 4721: 4719: 4718: 4712: 4706: 4697: 4691: 4679: 4678: 4672: 4660: 4659: 4650: 4644: 4638: 4632: 4617: 4616: 4610: 4604: 4598: 4583: 4582: 4577: 4571: 4565: 4560: 4548: 4547: 4541: 4535: 4529: 4523: 4517: 4505: 4504: 4499: 4488: 4487: 4486: 4472: 4458: 4442: 4439: 4435:price pressure 4420: 4417: 4391:safety factors 4355: 4352: 4328:Space Shuttle 4288: 4287: 4267: 4265: 4248: 4245: 4237:orbital energy 4233:kinetic energy 4221:Main article: 4218: 4215: 4196: 4192: 4156:orbital launch 4133: 4129: 4104: 4100: 4094: 4090: 4086: 4083: 4074: 4061: 4034: 4030: 4024: 4021: 4016: 4013: 4010: 4003: 4000: 3995: 3989: 3984: 3980: 3970: 3957: 3937: 3915: 3911: 3873: 3869: 3853:kinetic energy 3824: 3821: 3818: 3813: 3809: 3778: 3775: 3772: 3769: 3765: 3759: 3756: 3753: 3750: 3747: 3744: 3741: 3738: 3735: 3732: 3728: 3720: 3715: 3711: 3704: 3701: 3693: 3690: 3682: 3677: 3673: 3663: 3617:Main article: 3614: 3611: 3609: 3606: 3553: 3549: 3520: 3515: 3511: 3505: 3502: 3493: 3480: 3465:Main article: 3462: 3459: 3394:Main article: 3391: 3388: 3385: 3384: 3381: 3378: 3376: 3373: 3367: 3366: 3363: 3360: 3358: 3355: 3349: 3348: 3345: 3342: 3339: 3336: 3330: 3329: 3326: 3323: 3321: 3318: 3312: 3311: 3308: 3305: 3302: 3299: 3293: 3292: 3289: 3286: 3283: 3280: 3273: 3272: 3269: 3266: 3263: 3260: 3253: 3252: 3249: 3246: 3243: 3240: 3234: 3233: 3230: 3227: 3224: 3221: 3214: 3213: 3210: 3207: 3204: 3201: 3194: 3193: 3188: 3183: 3180: 3177: 3161:liquid methane 3115:Main article: 3112: 3109: 3088: 3084: 3078: 3074: 3023: 3020: 3011: 2996: 2992: 2982: 2967: 2963: 2953: 2938: 2934: 2924: 2920: 2919: 2904: 2900: 2894: 2890: 2884: 2881: 2876: 2872: 2868: 2862: 2859: 2830: 2826: 2788:Main article: 2785: 2782: 2766: 2763: 2759: 2733: 2729: 2719: 2704: 2701: 2697: 2687: 2670: 2666: 2662: 2657: 2654: 2650: 2646: 2641: 2637: 2627: 2612: 2609: 2605: 2584: 2583: 2580: 2571: 2563: 2562: 2559: 2550: 2542: 2541: 2538: 2533: 2525: 2524: 2521: 2517: 2509: 2507:liquid engines 2501: 2500: 2496: 2491: 2488: 2478: 2467:Main article: 2464: 2461: 2445: 2442: 2439: 2436: 2427: 2412: 2409: 2406: 2403: 2400: 2397: 2388: 2376:Main article: 2373: 2370: 2343: 2339: 2326:(m/s or ft/s). 2310: 2305: 2301: 2291: 2277: 2271: 2268: 2256: 2241: 2236: 2232: 2224: 2221: 2215: 2210: 2206: 2196: 2182: 2181: 2178: 2175: 2172: 2168: 2150: 2147: 2102:Drag (physics) 2097: 2094: 2090:launch vehicle 2049: 2048: 2039: 2033: 2024: 1990: 1987: 1908:Main article: 1905: 1902: 1900: 1897: 1858:Launch Pad 39A 1849: 1846: 1782:ground segment 1715: 1712: 1640:Main article: 1637: 1634: 1630:ejection seats 1555:pad abort test 1546: 1543: 1514:Main article: 1511: 1508: 1463: 1460: 1454:, such as the 1452:reconnaissance 1385: 1382: 1350: 1347: 1313: 1310: 1218:Main article: 1215: 1212: 1140:monopropellant 1128:jet propulsion 1109:Main article: 1106: 1103: 1028:rocket engines 1011: 1008: 999: 996: 995: 994: 989: 983:ejection seats 979: 973: 968: 963: 958: 948: 945: 940: 938:Apollo program 927: 922: 868: 867: 862: 859: 845:and later the 843:Project Gemini 804:Sergei Korolev 737:guided-missile 705:Test Stand VII 703:launched from 578:Hermann Oberth 564:Robert Goddard 517:William Leitch 314:Emperor Lizong 258:Main article: 255: 252: 232:monopropellant 190:ejection seats 85:jet propulsion 53:" (Site 1/5), 26: 9: 6: 4: 3: 2: 8700: 8689: 8686: 8684: 8681: 8679: 8676: 8674: 8671: 8669: 8666: 8664: 8661: 8660: 8658: 8643: 8639: 8634: 8632: 8623: 8622: 8619: 8613: 8610: 8608: 8605: 8603: 8600: 8598: 8595: 8594: 8592: 8590: 8586: 8580: 8577: 8575: 8572: 8570: 8567: 8565: 8561: 8558: 8556: 8553: 8551: 8550:Direct ascent 8548: 8547: 8545: 8543: 8539: 8533: 8532:Intergalactic 8530: 8528: 8525: 8523: 8520: 8516: 8513: 8511: 8508: 8507: 8506: 8503: 8501: 8498: 8497: 8495: 8491: 8483: 8480: 8478: 8475: 8473: 8470: 8468: 8467:Rocket engine 8465: 8464: 8463: 8460: 8456: 8453: 8451: 8448: 8446: 8443: 8441: 8438: 8436: 8433: 8431: 8428: 8427: 8426: 8423: 8421: 8418: 8414: 8411: 8409: 8406: 8404: 8401: 8400: 8399: 8398:Space capsule 8396: 8394: 8391: 8389: 8386: 8385: 8383: 8381: 8377: 8367: 8364: 8362: 8361:Space nursing 8359: 8357: 8354: 8352: 8349: 8345: 8342: 8341: 8340: 8337: 8335: 8332: 8328: 8325: 8324: 8323: 8320: 8319: 8317: 8315:Health issues 8313: 8307: 8304: 8302: 8299: 8297: 8294: 8292: 8289: 8287: 8284: 8280: 8277: 8276: 8275: 8272: 8270: 8269:Space Shuttle 8267: 8263: 8260: 8258: 8255: 8254: 8253: 8250: 8248: 8245: 8243: 8240: 8238: 8235: 8233: 8230: 8228: 8225: 8224: 8222: 8218: 8212: 8209: 8207: 8204: 8202: 8201:Space tourism 8199: 8197: 8194: 8192: 8189: 8187: 8184: 8182: 8179: 8175: 8172: 8170: 8167: 8165: 8162: 8161: 8160: 8157: 8153: 8150: 8149: 8148: 8145: 8144: 8142: 8138: 8135: 8133: 8129: 8123: 8122:Space weather 8120: 8118: 8115: 8113: 8110: 8108: 8105: 8103: 8100: 8098: 8095: 8093: 8090: 8088: 8085: 8081: 8078: 8076: 8073: 8071: 8068: 8066: 8063: 8062: 8061: 8058: 8054: 8051: 8049: 8046: 8044: 8041: 8039: 8036: 8035: 8034: 8031: 8029: 8026: 8025: 8023: 8021: 8017: 8009: 8006: 8005: 8004: 8001: 7997: 7994: 7992: 7989: 7987: 7986:Space command 7984: 7983: 7982: 7981:Space warfare 7979: 7975: 7972: 7970: 7967: 7965: 7962: 7960: 7957: 7955: 7952: 7951: 7950: 7947: 7943: 7942:United States 7940: 7938: 7935: 7933: 7930: 7928: 7925: 7923: 7920: 7918: 7915: 7913: 7910: 7908: 7905: 7903: 7900: 7899: 7898: 7895: 7893: 7890: 7886: 7883: 7881: 7878: 7876: 7873: 7871: 7868: 7867: 7866: 7863: 7861: 7860:Astrodynamics 7858: 7857: 7855: 7851: 7847: 7840: 7835: 7833: 7828: 7826: 7821: 7820: 7817: 7811: 7807: 7804: 7801: 7799: 7796: 7794: 7791: 7789: 7785: 7783: 7780: 7778: 7774: 7771: 7770: 7769: 7768: 7762: 7759: 7757: 7754: 7752: 7749: 7747: 7744: 7742: 7738: 7735: 7732: 7730: 7727: 7725: 7722: 7720: 7717: 7715: 7712: 7711: 7710: 7709: 7694: 7684: 7683: 7678: 7671: 7664: 7653: 7652: 7647: 7640: 7626:on 2013-12-10 7625: 7621: 7617: 7610: 7596: 7592: 7585: 7578: 7573: 7571: 7569: 7567: 7560: 7556: 7555:0-201-56751-2 7552: 7548: 7542: 7528:on 2012-04-25 7527: 7523: 7517: 7502: 7498: 7492: 7478:on 2011-04-27 7477: 7473: 7467: 7449: 7442: 7436: 7429: 7425: 7422: 7417: 7415: 7413: 7411: 7402: 7398: 7394: 7392:1-4244-0007-4 7388: 7384: 7380: 7376: 7372: 7365: 7349: 7345: 7341: 7335: 7320: 7316: 7310: 7295: 7291: 7285: 7271:on 2003-02-04 7270: 7266: 7260: 7246:on 2002-06-25 7245: 7241: 7235: 7221:on 2016-06-02 7220: 7216: 7212: 7209:NASA (2006). 7205: 7191:on 2013-12-06 7187: 7180: 7174: 7172: 7170: 7168: 7166: 7157: 7153: 7147: 7139: 7135: 7129: 7127: 7118: 7114: 7108: 7106: 7097: 7093: 7087: 7085: 7070:on 2013-02-16 7069: 7065: 7059: 7045:on 2013-01-08 7044: 7040: 7034: 7019: 7015: 7009: 6994: 6990: 6984: 6976: 6972: 6966: 6958: 6954: 6947: 6945: 6943: 6941: 6926:on 2016-06-17 6925: 6921: 6920:"Mach 1 Club" 6915: 6901:on 2011-07-22 6900: 6896: 6890: 6875: 6869: 6867: 6858: 6857: 6849: 6833: 6829: 6825: 6821: 6820: 6812: 6798:on 2012-11-29 6797: 6793: 6787: 6779: 6773: 6769: 6765: 6764: 6756: 6741: 6737: 6729: 6721: 6715: 6711: 6707: 6706: 6698: 6683:on 2011-06-29 6682: 6678: 6672: 6657:on 2017-03-02 6653: 6646: 6640: 6629: 6625: 6621: 6614: 6613: 6605: 6603: 6601: 6586: 6582: 6578: 6574: 6568: 6554:on 2020-09-25 6553: 6549: 6545: 6539: 6523: 6519: 6518:Evening Times 6515: 6508: 6492: 6491: 6486: 6480: 6464: 6463: 6458: 6452: 6438:on 2013-06-02 6437: 6433: 6427: 6411: 6405: 6389: 6385: 6379: 6368: 6362: 6348:on 2012-04-10 6347: 6343: 6339: 6335: 6329: 6315:on 2014-02-07 6314: 6310: 6304: 6290:on 2014-02-05 6289: 6285: 6281: 6275: 6261:on 2010-04-06 6260: 6256: 6249: 6233: 6229: 6225: 6218: 6202: 6198: 6194: 6188: 6180: 6174: 6170: 6169: 6161: 6145: 6141: 6137: 6130: 6114: 6110: 6106: 6099: 6085:on 2014-08-05 6084: 6080: 6074: 6072: 6056: 6052: 6046: 6032:on 2013-09-11 6031: 6027: 6021: 6006: 6002: 5996: 5980: 5976: 5969: 5962: 5946: 5942: 5935: 5927: 5920: 5912: 5910:0-87614-863-1 5906: 5902: 5897: 5896: 5887: 5873:on 2021-10-30 5872: 5868: 5864: 5863: 5858: 5852: 5841: 5834: 5833: 5826: 5812:on 2008-01-14 5811: 5807: 5800: 5787:on 2009-06-18 5786: 5782: 5778: 5774: 5773: 5768: 5761: 5753: 5746: 5732:on 2010-02-13 5731: 5727: 5721: 5713: 5707: 5703: 5696: 5688: 5682: 5678: 5671: 5656: 5652: 5648: 5641: 5627:on 2013-01-25 5626: 5622: 5616: 5600: 5593: 5577: 5573: 5571:9780029228951 5567: 5563: 5558: 5557: 5548: 5541: 5535: 5520: 5516: 5510: 5495: 5491: 5485: 5478: 5472: 5471:DGA Quarterly 5468: 5461: 5454: 5450: 5445: 5443: 5427: 5423: 5417: 5409: 5408: 5400: 5385: 5381: 5374: 5367: 5363: 5356: 5355: 5350: 5344: 5342: 5334: 5328: 5320: 5319: 5311: 5303: 5302: 5294: 5278: 5271: 5256: 5252: 5245: 5230: 5226: 5222: 5216: 5208: 5202: 5198: 5190: 5177: 5171: 5167: 5163: 5159: 5158:Genesis Redux 5155: 5148: 5140: 5134: 5130: 5123: 5115: 5111: 5107: 5103: 5099: 5092: 5077: 5073: 5069: 5065: 5059: 5043: 5039: 5035: 5031: 5025: 5016: 5008: 5002: 4998: 4991: 4984: 4974:on 2006-08-05 4973: 4969: 4965: 4959: 4945:on 2009-07-09 4944: 4940: 4936: 4929: 4913: 4909: 4903: 4899: 4898: 4890: 4888: 4886: 4884: 4882: 4880: 4878: 4876: 4874: 4872: 4870: 4868: 4866: 4864: 4862: 4860: 4858: 4856: 4854: 4852: 4836: 4830: 4826: 4821: 4820: 4811: 4809: 4804: 4793: 4760: 4751: 4744: 4743: 4738: 4732: 4728: 4716: 4713: 4710: 4707: 4701: 4698: 4695: 4692: 4689: 4686: 4685: 4684: 4683: 4682:Miscellaneous 4676: 4673: 4670: 4667: 4666: 4665: 4664: 4654: 4653:VA-111 Shkval 4651: 4648: 4645: 4642: 4639: 4636: 4633: 4627: 4624: 4623: 4622: 4621: 4614: 4611: 4608: 4605: 4602: 4599: 4594: – Hobby 4593: 4590: 4589: 4588: 4587: 4581: 4578: 4575: 4572: 4569: 4566: 4564: 4561: 4558: 4555: 4554: 4553: 4552: 4545: 4542: 4539: 4536: 4533: 4530: 4527: 4526:Rocket garden 4524: 4521: 4518: 4515: 4512: 4511: 4510: 4509: 4503: 4500: 4498: 4495: 4494: 4493: 4492: 4484: 4473: 4470: 4459: 4456: 4445: 4438: 4436: 4432: 4426: 4416: 4414: 4409: 4406: 4404: 4400: 4395: 4392: 4387: 4384: 4380: 4375: 4373: 4369: 4365: 4364:Space Shuttle 4359: 4351: 4349: 4348:Space Shuttle 4343: 4341: 4337: 4333: 4331: 4325: 4321: 4316: 4310: 4306: 4305: 4299: 4298:Space Shuttle 4294: 4284: 4275: 4271: 4268:This section 4266: 4263: 4259: 4258: 4254: 4244: 4240: 4238: 4234: 4230: 4224: 4223:Oberth effect 4217:Oberth effect 4214: 4212: 4194: 4190: 4181: 4176: 4173: 4169: 4165: 4164:Space Shuttle 4161: 4157: 4153: 4148: 4131: 4127: 4102: 4098: 4092: 4088: 4084: 4081: 4073: 4059: 4032: 4022: 4019: 4011: 4008: 4001: 3998: 3993: 3987: 3982: 3978: 3969: 3955: 3935: 3913: 3909: 3895: 3891: 3887: 3871: 3867: 3858: 3854: 3850: 3845: 3843: 3838: 3819: 3816: 3811: 3807: 3799: 3776: 3773: 3770: 3767: 3763: 3757: 3754: 3751: 3748: 3745: 3742: 3739: 3736: 3733: 3730: 3726: 3718: 3713: 3709: 3702: 3699: 3691: 3688: 3680: 3675: 3671: 3662: 3659: 3657: 3652: 3650: 3646: 3637: 3636: 3630: 3629:Space Shuttle 3625: 3620: 3605: 3603: 3599: 3595: 3590: 3588: 3584: 3580: 3575: 3571: 3567: 3551: 3547: 3518: 3513: 3509: 3503: 3500: 3492: 3478: 3468: 3458: 3454: 3452: 3448: 3444: 3439: 3437: 3432: 3430: 3426: 3422: 3414: 3410: 3402: 3397: 3382: 3379: 3377: 3374: 3372: 3369: 3368: 3364: 3361: 3359: 3356: 3354: 3351: 3350: 3346: 3343: 3340: 3337: 3335: 3332: 3331: 3327: 3324: 3322: 3319: 3317: 3314: 3313: 3309: 3306: 3303: 3300: 3298: 3295: 3294: 3290: 3287: 3284: 3281: 3279:(stage only) 3278: 3275: 3274: 3270: 3267: 3264: 3261: 3258: 3257:Space Shuttle 3255: 3254: 3250: 3247: 3244: 3241: 3239: 3236: 3235: 3231: 3228: 3225: 3222: 3219: 3216: 3215: 3211: 3208: 3205: 3202: 3199: 3196: 3195: 3192: 3191:Mass fraction 3189: 3187: 3184: 3181: 3179:Takeoff mass 3178: 3175: 3174: 3171: 3168: 3166: 3162: 3158: 3154: 3149: 3146: 3144: 3140: 3136: 3131: 3123: 3118: 3108: 3106: 3086: 3082: 3076: 3072: 3060: 3058: 3054: 3050: 3046: 3041: 3021: 2994: 2990: 2965: 2961: 2936: 2932: 2923: 2902: 2898: 2892: 2888: 2882: 2879: 2874: 2870: 2866: 2860: 2850: 2849: 2848: 2846: 2828: 2824: 2814: 2812: 2805: 2801: 2796: 2791: 2781: 2764: 2761: 2757: 2731: 2727: 2702: 2699: 2695: 2686: 2668: 2664: 2660: 2655: 2652: 2648: 2644: 2639: 2635: 2626: 2610: 2607: 2603: 2594: 2589: 2581: 2579: 2575: 2572: 2570: 2565: 2564: 2560: 2558: 2554: 2551: 2549: 2546:Space Shuttle 2544: 2543: 2539: 2537: 2534: 2532: 2529:Space Shuttle 2527: 2526: 2522: 2520: 2513: 2510: 2508: 2505:Space Shuttle 2503: 2502: 2499:, vacuum (s) 2495: 2492: 2489: 2486: 2485: 2481: 2477: 2470: 2460: 2443: 2440: 2437: 2434: 2426: 2410: 2407: 2404: 2401: 2398: 2395: 2387: 2385: 2379: 2372:Total impulse 2369: 2367: 2365: 2358: 2341: 2337: 2325: 2308: 2303: 2299: 2275: 2269: 2266: 2255: 2239: 2234: 2230: 2222: 2219: 2213: 2208: 2204: 2195: 2192: 2190: 2179: 2176: 2173: 2171:Underexpanded 2170: 2169: 2166: 2162: 2156: 2146: 2144: 2140: 2135: 2133: 2129: 2125: 2120: 2118: 2117:drag equation 2111: 2107: 2103: 2093: 2091: 2087: 2083: 2079: 2075: 2071: 2070: 2064: 2063:is obtained. 2062: 2058: 2054: 2047: 2043: 2040: 2037: 2034: 2032: 2028: 2025: 2022: 2019: 2018: 2017: 2014: 2012: 2011:astrodynamics 2008: 2004: 1995: 1986: 1984: 1983: 1978: 1974: 1969: 1966: 1960: 1952: 1948: 1946: 1942: 1938: 1934: 1930: 1925: 1916: 1911: 1910:Rocket engine 1896: 1894: 1888: 1884: 1881: 1880:Space Shuttle 1876: 1874: 1870: 1866: 1859: 1854: 1845: 1843: 1839: 1820: 1816: 1813: 1809: 1805: 1800: 1796: 1794: 1790: 1785: 1783: 1779: 1775: 1771: 1767: 1763: 1758: 1756: 1752: 1749:Launches for 1745: 1741: 1740: 1734: 1733:Space Shuttle 1711: 1708: 1706: 1702: 1698: 1694: 1690: 1688: 1684: 1679: 1676: 1672: 1666: 1664: 1660: 1656: 1651: 1649: 1643: 1633: 1631: 1626: 1624: 1623:space station 1621: 1617: 1612: 1610: 1606: 1605:3L, 5L and 7L 1602: 1598: 1593: 1591: 1587: 1583: 1578: 1576: 1572: 1568: 1567:Breeches buoy 1560: 1556: 1551: 1542: 1540: 1536: 1532: 1528: 1523: 1517: 1507: 1505: 1500: 1498: 1494: 1490: 1486: 1479: 1474: 1469: 1459: 1457: 1453: 1449: 1445: 1441: 1437: 1433: 1432: 1427: 1423: 1419: 1418: 1413: 1405: 1400: 1395: 1391: 1381: 1378: 1376: 1372: 1368: 1364: 1360: 1356: 1346: 1344: 1340: 1336: 1335:rocket engine 1332: 1328: 1318: 1309: 1307: 1302: 1300: 1296: 1292: 1287: 1285: 1284:catalytically 1281: 1277: 1276:nitrous oxide 1273: 1268: 1266: 1262: 1261:liquid oxygen 1258: 1254: 1250: 1246: 1243: 1239: 1238:rocket engine 1235: 1226: 1221: 1211: 1209: 1205: 1201: 1197: 1193: 1189: 1185: 1181: 1177: 1173: 1169: 1165: 1164:steam rockets 1161: 1157: 1153: 1149: 1145: 1141: 1137: 1133: 1132:Rocket engine 1129: 1122:rocket engine 1121: 1117: 1112: 1111:Rocket engine 1102: 1100: 1096: 1092: 1088: 1084: 1080: 1076: 1072: 1067: 1065: 1061: 1057: 1053: 1049: 1045: 1041: 1037: 1033: 1029: 1025: 1021: 1017: 1007: 1005: 993: 990: 988: 984: 980: 978: 974: 972: 969: 967: 966:rocket trains 964: 962: 959: 956: 952: 949: 946: 944: 941: 939: 936:used for the 935: 931: 930:space rockets 928: 926: 923: 921: 917: 913: 909: 908:water rockets 905: 901: 900: 899: 893: 889: 885: 882: 865: 864: 858: 856: 852: 848: 844: 840: 836: 832: 828: 824: 820: 816: 812: 807: 806:(1907–1966). 805: 801: 797: 793: 792:sound barrier 789: 785: 781: 777: 773: 768: 766: 762: 758: 754: 750: 749:Bachem Ba 349 746: 742: 738: 734: 730: 726: 722: 718: 714: 706: 702: 698: 694: 691: 687: 686: 681: 677: 673: 669: 668: 663: 658: 656: 652: 648: 644: 640: 636: 633:In 1921, the 628: 624: 619: 615: 613: 609: 605: 601: 597: 593: 589: 585: 584: 579: 575: 574: 569: 565: 556: 552: 550: 546: 542: 541:Archibald Low 538: 534: 529: 527: 523: 518: 514: 512: 508: 504: 500: 496: 495:William Moore 491: 489: 485: 481: 477: 473: 466: 462: 458: 454: 450: 448: 444: 440: 432: 428: 424: 420: 418: 414: 410: 406: 402: 398: 394: 391: 386: 384: 380: 377:around 1405. 376: 375: 370: 369:Konrad Kyeser 366: 362: 361: 356: 352: 348: 344: 340: 335: 333: 329: 325: 321: 320: 315: 311: 307: 303: 299: 295: 291: 287: 279: 278: 272: 267: 261: 251: 249: 245: 241: 237: 233: 229: 225: 221: 217: 213: 209: 207: 203: 199: 195: 191: 187: 183: 179: 175: 171: 167: 162: 160: 156: 152: 148: 144: 140: 136: 132: 128: 127:accelerations 124: 120: 116: 112: 110: 106: 102: 98: 97:rocket engine 94: 90: 86: 82: 76: 71: 67: 63: 56: 52: 48: 43: 39: 35: 30: 19: 18:Rocket launch 8542:Space launch 8527:Interstellar 8493:Destinations 8392: 8262:Apollo–Soyuz 8211:Space diving 8196:Space toilet 8020:Applications 7937:Soviet Union 7897:Space policy 7892:Space launch 7766: 7765: 7707: 7706: 7692: 7686:. Retrieved 7680: 7670: 7661: 7655:. Retrieved 7649: 7639: 7628:. Retrieved 7624:the original 7619: 7609: 7598:. Retrieved 7594: 7584: 7546: 7541: 7530:. Retrieved 7526:the original 7516: 7505:. Retrieved 7491: 7480:. Retrieved 7476:the original 7466: 7455:. Retrieved 7448:the original 7435: 7374: 7364: 7352:. Retrieved 7348:the original 7334: 7323:. Retrieved 7309: 7298:. Retrieved 7284: 7273:. Retrieved 7269:the original 7259: 7248:. Retrieved 7244:the original 7234: 7223:. Retrieved 7219:the original 7214: 7204: 7193:. Retrieved 7186:the original 7156:the original 7146: 7138:the original 7117:the original 7096:the original 7072:. Retrieved 7068:the original 7058: 7047:. Retrieved 7043:the original 7033: 7022:. Retrieved 7008: 6997:. Retrieved 6983: 6975:the original 6965: 6956: 6928:. Retrieved 6924:the original 6914: 6903:. Retrieved 6899:the original 6889: 6878:. Retrieved 6855: 6848: 6836:. Retrieved 6818: 6811: 6800:. Retrieved 6796:the original 6786: 6762: 6755: 6743:. 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Index

Rocket launch
Rocket (disambiguation)

Soyuz-FG
Gagarin's Start
Baikonur Cosmodrome
Italian
lit.
vehicle
jet propulsion
accelerate
air
rocket engine
reaction
propellant
vacuum
Multistage rockets
escape velocity
airbreathing engines
accelerations
momentum
airfoils
auxiliary reaction engines
gimballed thrust
momentum wheels
deflection of the exhaust stream
spin
gravity
China
Space Age

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