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Ejection seat

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528: 448: 710: 181: 519:. All three, after ejection, would be propelled by small turbojet engine developed for target drones. With the exception of the Kaman design, the pilot would still be required to parachute to the ground after reaching a safety-point for rescue. The AERCAB project was terminated in the 1970s with the end of the Vietnam War. The Kaman design, in early 1972, was the only one which was to reach the hardware stage. It came close to being tested with a special landing-gear platform attached to the AERCAB ejection seat for first-stage ground take offs and landings with a test pilot. 912:), specifically from aircraft cockpits. The zero-zero capability was developed to help aircrews escape upward from unrecoverable emergencies during low-altitude and/or low-speed flight, as well as ground mishaps. Parachutes require a minimum altitude for opening, to give time for deceleration to a safe landing speed. Thus, prior to the introduction of zero-zero capability, ejections could only be performed above minimum altitudes and airspeeds. If the seat was to work from zero (aircraft) altitude, the seat would have to lift itself to a sufficient altitude. 832:
away from the stricken craft on a guide rail. Some operate like a standard ejector seat, by jettisoning the canopy, then deploying a drag chute into the airflow. That chute pulls the occupant out of the aircraft, either with the seat or following release of the seat straps, who then rides off the end of a rail extending far enough out to help clear the structure. In the case of the Space Shuttle, the astronauts would have ridden a long, curved rail, blown by the wind against their bodies, then deployed their chutes after free-falling to a safe altitude.
807:", strikes the underside of the canopy and shatters it. The A-10 Thunderbolt II is equipped with canopy breakers on either side of its headrest in the event that the canopy fails to jettison. The T-6 is also equipped with such breakers if the MDC fails to detonate. In ground emergencies, a ground crewman or pilot can use a breaker knife attached to the inside of the canopy to shatter the transparency. The A-6 Intruder and EA-6B Prowler seats were capable of ejecting through the canopy, with canopy jettison a separate option if there is enough time. 887: 792: 836: 637: 32: 129: 698: 402: 503:(AERCAB) ejection seats (both terms have been used by the US military and defence industry), where after the pilot ejected, the ejection seat would fly them to a location far enough away from where they ejected to where they could safely be picked up. A Request for Proposals for concepts for AERCAB ejection seats were issued in the late 1960s. Three companies submitted papers for further development: A 1756: 192: 547: 623:
secondary handle in the front of the seat to allow ejection even when pilots weren't able to reach upwards because of high g-force. Later (e.g. in Martin Baker's MK9) the top handle was discarded because the lower handle had proven easier to operate and the technology of helmets had advanced to also protect from the air blast.
752:. In order to make this work, the pilot was equipped with "spurs" which were attached to cables that would pull the legs inward so the pilot could be ejected. Following this development, some other egress systems began using leg retractors as a way to prevent injuries to flailing legs, and to provide a more stable 858:
supersonic bombers. These seats were enclosed in an air-operated clamshell, which permitted the aircrew to escape at airspeeds and altitudes high enough to otherwise cause bodily harm. These seats were designed to allow the pilot to control the plane even with the clamshell closed, and the capsule
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Drag Extraction is the lightest and simplest egress system available, and has been used on many experimental aircraft. Halfway between simply "bailing out" and using explosive-eject systems, Drag Extraction uses the airflow past the aircraft (or spacecraft) to move the aviator out of the cockpit and
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The "standard" ejection system operates in two stages. First, the entire canopy or hatch above the aviator is opened, shattered, or jettisoned, and the seat and occupant are launched through the opening. In most earlier aircraft this required two separate actions by the aviator, while later egress
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K-36DM ejection seat and the pilot is wearing the КО-15 protective gear, they are able to eject at airspeeds from 0 to 1,400 kilometres per hour (870 mph) and altitudes of 0 to 25 km (16 mi or about 82,000 ft). The K-36DM ejection seat features drag chutes and a small shield that
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Similarly, two of the six ejection seats on the B-52 Stratofortress fire downward, through hatch openings on the bottom of the aircraft; the downward hatches are released from the aircraft by a thruster that unlocks the hatch, while gravity and wind remove the hatch and arm the seat. The four seats
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As of 20 June 2011 – when two Spanish Air Force pilots ejected over San Javier airport – the number of lives saved by Martin-Baker products was 7,402 from 93 air forces. The company runs a club called the "Ejection Tie Club" and gives survivors a unique tie and lapel pin. The total figure
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was the first aircraft to be fitted with a rocket-propelled seat. Martin-Baker developed a similar design, using multiple rocket units feeding a single nozzle. The greater thrust from this configuration had the advantage of being able to eject the pilot to a safe height even if the aircraft was on
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line of aircraft) use Canopy Destruct systems, which have an explosive cord (MDC – Miniature Detonation Cord or FLSC – Flexible Linear Shaped Charge) embedded within the acrylic plastic of the canopy. The MDC is initiated when the eject handle is pulled, and shatters the canopy over the seat a few
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The ACES II ejection seat is used in most American-built fighters. The A-10 uses connected firing handles that activate both the canopy jettison systems, followed by the seat ejection. The F-15 has the same connected system as the A-10 seat. Both handles accomplish the same task, so pulling either
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at an altitude of 80,000 ft (24,000 m). The pilot was recovered successfully, but the launch control officer drowned after a water landing. Despite these records, most ejections occur at fairly low speeds and altitudes, when the pilot can see that there is no hope of regaining aircraft
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canopy quickly for a successful parachute descent, so that proper deployment of the parachute no longer relies on airspeed and altitude. The seat cannon clears the seat from the aircraft, then the under-seat rocket pack fires to lift the seat to altitude. As the rockets fire for longer than the
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Early seats used a solid propellant charge to eject the pilot and seat by igniting the charge inside a telescoping tube attached to the seat. As aircraft speeds increased still further, this method proved inadequate to get the pilot sufficiently clear of the airframe. Increasing the amount of
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Early models of the ejection seat were equipped with only an overhead ejection handle which doubled in function by forcing the pilot to assume the right posture and by having them pull a screen down to protect both their face and oxygen mask from the subsequent air blast. Martin Baker added a
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The minimal ejection altitude for ACES II seat in inverted flight is about 140 feet (43 m) above ground level at 150 KIAS, while the Russian counterpart – K-36DM has the minimal ejection altitude from inverted flight of 100 feet (30 m) AGL. When an aircraft is equipped with the
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C tugs in a heavy snow-shower. At 7,875 ft (2,400 m), Schenk found he had no control, jettisoned his towline, and ejected. The He 280 was never put into production status. The first operational type built anywhere to provide ejection seats for the crew was the
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in 1940. One of the He 280 test pilots, Helmut Schenk, became the first person to escape from a stricken aircraft with an ejection seat on 13 January 1942 after his control surfaces iced up and became inoperative. The fighter was being used in tests of the
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shells, were placed in the bottom of the pipes, facing upward. When fired, the gases would fill the pipes, "popping" the caps off the end, and thereby forcing the seat to ride up the pipes on its wheels and out of the aircraft. By the end of the war, the
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on the forward upper deck (two of them, EWO and Gunner, facing the rear of the airplane) fire upwards as usual. Any such downward-firing system is of no use on or near the ground if aircraft is in level flight at the time of the ejection.
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Air Pageant in 1948, ejecting from a Meteor. Martin-Baker ejector seats were fitted to prototype and production aircraft from the late 1940s, and the first emergency use of such a seat occurred in 1949 during testing of the jet-powered
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became concerned about its pilots ejecting over hostile territory and those pilots either being captured or killed and the losses in men and aircraft in attempts to rescue them. Both services began a program titled
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needed over the very short length on the cannon barrel within the seat. This limited the total energy, and thus the additional height possible, as otherwise the high forces needed would crush the pilot.
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aircraft as ejection may be necessary while the aircraft was in the hover, and jettisoning the canopy might result in the pilot and seat striking it. This system is also used in the
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Aircraft designed for low-level use sometimes have ejection seats which fire through the canopy, as waiting for the canopy to be ejected is too slow. Many aircraft types (e.g., the
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had ditched on launch and been cut in two by the carrier on 13 October 1954. Documented evidence also exists that pilots of the US and Indian navies have also performed this feat.
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Pilots have successfully ejected from underwater in a handful of instances, after being forced to ditch in water. The first recorded case was Lt. B. D. Macfarlane of the
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cannon, they do not require the same high forces. Zero-zero rocket seats also reduced forces on the pilot during any ejection, reducing injuries and spinal compression.
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located at the aft end of the fuselage presenting a hazard to a normal "bailout" escape—and a few late-war prototype aircraft were also fitted with ejection seats.
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on 27 February 1944, and the first real use occurred by Lt. Bengt Johansson on 29 July 1946 after a mid-air collision between a J 21 and a J 22.
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A warning applied on the cockpit side of some aircraft using an ejection seat system intended especially for the maintenance and emergency crews
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jet. Shortly afterward, on 17 August 1946, 1st Sgt. Larry Lambert was the first live U.S. ejectee. Lynch demonstrated the ejection seat at the
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After World War II, the need for such systems became pressing, as aircraft speeds were getting ever higher, and it was not long before the
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Modern zero-zero technology use small rockets to propel the seat upward to an adequate altitude and a small explosive charge to open the
866:, do not have individual ejection seats, but instead, the entire section of the airframe containing the crew can be ejected as a single 730:
one suffices. The F-16 has only one handle located between the pilot's knees, since the cockpit is too narrow for side-mounted handles.
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of an aircraft (usually military) in an emergency. In most designs, the seat is propelled out of the aircraft by an explosive charge or
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No real life land vehicle has ever been fitted with an ejection seat, though it is a common trope in fiction. A notable example is the
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A zero-zero ejection seat is designed to safely extract upward and land its occupant from a grounded stationary position (i.e., zero
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In the early 1960s, deployment of rocket-powered ejection seats designed for use at supersonic speeds began in such planes as the
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The first live flight test of the Martin-Baker system took place on 24 July 1946, when fitter Bernard Lynch ejected from a
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system designs, such as the Advanced Concept Ejection Seat model 2 (ACES II), perform both functions as a single action.
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were planned to be fitted with K-36RB (K-36M-11F35) seats, but as the program was canceled, the seats were never used.
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were equipped with ejection seats which were automatically activated during at least some part of the flight envelope.
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system is used to cushion the landing, and this also acts as a flotation device if the Crew Capsule lands in water.
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Non-standard egress systems include Downward Track (used for some crew positions in bomber aircraft, including the
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Through-Canopy Penetration is similar to Canopy Destruct, but a sharp spike on the top of the seat, known as the "
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The purpose of an ejection seat is pilot survival. The pilot typically experiences an acceleration of about 12–14
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It was theorised early on that ejection at supersonic speeds would be unsurvivable; extensive tests, including
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with an ejection seat. The system is similar to that of a conventional fixed-wing aircraft; however the main
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In Sweden, a version using compressed air was tested in 1941. A gunpowder ejection seat was developed by
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As the first operational military jet in late 1944 to ever feature one, the winner of the German
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when he successfully ejected under water using his Martin-Baker Mk.1 ejection seat after his
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An Aviation Structural Mechanic works on an ejection seat removed from the cockpit of an
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CD and TCP systems cannot be used with canopies made of flexible materials, such as the
2466: 2446: 2441: 2415: 2326: 2267: 2039: 970:, (LLRV) and its successor Lunar Landing Training Vehicle (LLTV), used ejection seats. 475: 352: 237: 1585: 940:, which entered limited service with Russian forces in 1995, was the first production 2870: 2774: 2511: 2456: 2436: 2366: 2361: 2346: 2034: 1724: 1693: 1387: 1281: 1249:"flight july | expressat gatwick | a/r d/wl | 1948 | 1092 |" 1178: 1081: 1076: 916: 785: 753: 745: 722: 574: 436: 229: 474:
bomber in 1958). Following an accident on 30 July 1966 in the attempted launch of a
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Nouveau système de montage des parachutes dans les appareils de locomotion aérienne
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Space Shuttle – The History of Developing the National Space Transportation System
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The modern layout for an ejection seat was first introduced by Romanian inventor
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These early seats were fired from the aircraft with a cannon, providing the high
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as it rolls into the carrier's catwalk after a brake failure on the deck of the
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The first ejection seats were developed independently during World War II by
252:. Dragomir patented his "catapult-able cockpit" at the French Patent Office. 1481: 955:
The only commercial jetliner ever fitted with ejection seats was the Soviet
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milliseconds before the seat is launched. This system was developed for the
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for all types of ejection seats is unknown, but may be considerably higher.
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were equipped with a Downward Track ejection seat due to the hazard of the
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Bull, John O.; Serocki, Edward L.; McDowell, Howard L. (September 1966).
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Pilot ejecting from A-6 Intruder after failed aircraft carrier landing
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ejected on 6 May 1968, following Joe Algranti and Stuart M. Present.
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propellant risked damaging the occupant's spine, so experiments with
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was broken. Manual escape at such speeds would be impossible. The
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The only spacecraft ever flown with installed ejection seats were
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test subjects, were undertaken to determine that it was feasible.
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rises between the pilot's legs to deflect air around the pilot.
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Encapsulated Seat egress systems were developed for use in the
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experimented with downward-ejecting systems operated by a
168:) Once clear of the aircraft, the ejection seat deploys a 160:, carrying the pilot with it. The concept of an ejectable 1620:. Martin-Baker. pp. 4, 17, 19, 36–37. Archived from 1470:
ejection-history.org.uk Aircraft by Type: Westland Wyvern
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was a production model, and did not have ejection seats.
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to jettison the blades moments before the seat is fired.
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of vertebrae are a recurrent side effect of ejection.
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on 2 July 1970. The pilot was recovered by helicopter.
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Historical Division, Office of Information Services
56:. Unsourced material may be challenged and removed. 19:"Ejector seat" redirects here. For other uses, see 1717:Terry, Gerard (August–November 1984). "Talkback". 1857:"In Pictures: A Potted History Of Ejection Seats" 1820:"IN PICTURES: Lethbridge CF-18 jet fighter crash" 1038:Further information on the flight simulator: 961:Tu-144 that crashed at the Paris Air Show in 1973 2852: 490:Late in the Vietnam War, the U.S. Air Force and 1710: 1369: 1305:. Hearst Magazines. September 1969. p. 90. 992:Early flights of the Space Shuttle, which used 1903: 1692:. Dennis R. Jenkins Publishing. p. 272. 872:Launch Escape System of the Apollo spacecraft 1830: 1278:Lockheed's Blackbirds: A-12, YF-12 and SR-71 1127:He later changed his surname to Järkenstedt. 713:Capt. Christopher Stricklin ejects from his 592:fighters ejected after a mid-air collision. 301:turbojets removed, and was towed aloft from 795:The ACES II Ejection seat commonly used on 665:. Unsourced material may be challenged and 1910: 1896: 1796: 881: 1561:"PARIS: Martin-Baker seats save in Spain" 1151:. Ejection-history.org.uk. Archived from 685:Learn how and when to remove this message 584:were unintentionally demonstrated at the 531:Lt. (j.g.) William Belden ejects from an 232:in the late 1920s. The design featured a 116:Learn how and when to remove this message 1505: 1382:, Air Research and Development Command, 1317:"1972 | 0502 | Flight Archive" 1270: 1177:. New York: Galahad Books. p. 363. 1035:, which had an ejecting passenger seat. 885: 834: 790: 708: 696: 545: 526: 446: 400: 190: 179: 127: 1760:Martin Baker Mk 1 ejection seat drawing 1749:Martin Baker Mk 1 ejection seat drawing 1687: 1681: 859:would float in case of water landings. 588:on 24 July 1993 when the pilots of two 487:control before impact with the ground. 2853: 1875:. Air Force Flight Dynamics Laboratory 1806:Kalei, Kalikiano (February 27, 2008). 1417:"The Mig-29 crash at Fairford Airbase" 721:ejection seat on 14 September 2003 at 332:. The first test in the air was on a 307:central test facility of the Luftwaffe 1891: 1805: 1716: 1484:. The Ejection Site. April 15, 1997. 1172: 1115:Patent no. 678566, of April 2, 1930, 1380:Air Force Missile Development Center 1166: 1102: 663:adding citations to reliable sources 630: 54:adding citations to reliable sources 25: 862:Some aircraft designs, such as the 725:, Idaho. Stricklin was not injured. 501:Aerial Escape and Rescue Capability 148:is a system designed to rescue the 13: 1530:"Navy's first underwater ejection" 14: 2892: 1736: 931: 824:naval fighter planes such as the 626: 497:Air Crew Escape/Rescue Capability 221:, patented an ejector seat using 1754: 1563:. Flight Global. June 21, 2011. 1319:. Flightglobal.com. 1972-03-02. 1255:. Flightglobal.com. 1948-07-15. 1175:The Warplanes of the Third Reich 1020:fitted with ejection seats. The 635: 371:powering the design) powering a 255:The design was perfected during 30: 16:Emergency aircraft escape system 1670:from the original on 2013-04-03 1656: 1645:from the original on 2012-12-28 1639:"Watch Neil Armstrong Narrowly" 1631: 1607: 1596:from the original on 2016-11-02 1578: 1567:from the original on 2016-10-31 1553: 1542:from the original on 2016-10-31 1522: 1499: 1488:from the original on 2012-04-07 1474: 1463: 1452:from the original on 2016-10-31 1434: 1423:from the original on 2018-02-06 1409: 1398:from the original on 2015-05-01 1363: 1352:from the original on 2016-10-31 1334: 1323:from the original on 2012-11-02 1309: 1259:from the original on 2012-11-06 1230:from the original on 2011-09-27 1205:from the original on 2012-07-16 522: 297:development. It had its usual 41:needs additional citations for 2820:In-flight entertainment system 2517:Horizontal situation indicator 1831:Bennett, Michael (1980–2014). 1291: 1241: 1216: 1191: 1141: 1121: 1109: 968:Lunar Landing Research Vehicle 1: 1506:Pasricha, Vinod (June 1986). 384:United States Army Air Forces 21:Ejector seat (disambiguation) 2800:Environmental control system 1786:"Safety for Service Aircrew" 1711:General and cited references 1134: 7: 1723:. No. 25. p. 79. 1688:Jenkins, Dennis R. (1999). 1044: 328:and tested in 1943 for the 201:ejection seat test using a 10: 2897: 2866:Aircraft emergency systems 2477:Course deviation indicator 2168:Electro-hydraulic actuator 1797:Coyne, Kevin (1996–2003). 1037: 507:design by Bell Systems; a 441:Convair F-102 Delta Dagger 425:Armstrong Whitworth A.W.52 175: 164:has also been tried. (See 18: 2767: 2746: 2708:Conventional landing gear 2679: 2575: 2410: 2276: 2113: 1929: 1753: 1748: 1743: 1442:"Ejection seat К-36D-3,5" 893:DM Ejection seat used on 817:canopy used on the F-16. 444:or very near the ground. 390:, but it was the work of 2492:Flight management system 1370:Bushnell, David (1958). 1097: 580:The capabilities of the 482:crew members ejected at 468:Convair F-106 Delta Dart 309:in Germany by a pair of 305:Erprobungsstelle Rechlin 2795:Emergency oxygen system 2557:Turn and slip indicator 2352:Leading-edge droop flap 2322:Drag-reducing aerospike 2297:Adaptive compliant wing 2292:Active Aeroelastic Wing 1384:Holloman Air Force Base 1346:Naval Historical Center 1173:Green, William (1986). 1051:Attacks on parachutists 882:Zero-zero ejection seat 797:United States Air Force 774:Hawker Siddeley Harrier 321:night fighter in 1942. 244:and in October 1929 at 217:, an early inventor of 196:United States Air Force 2835:Passenger service unit 2636:Self-sealing fuel tank 2532:Multi-function display 1535:The New Indian Express 1419:. Sirviper.com. 2006. 1062:Dynamic response index 1018:Space Shuttle orbiters 901: 864:General Dynamics F-111 847: 800: 726: 702: 551: 543: 463: 409: 206: 188: 133: 132:Various ejection seats 2815:Ice protection system 2733:Tricycle landing gear 2723:Landing gear extender 1940:Aft pressure bulkhead 1508:"Aircraft Underwater" 1482:"Underwater Ejection" 889: 838: 794: 712: 700: 564:Compression fractures 549: 530: 450: 439:began. In 1958, the 414:Gloster Meteor Mk III 404: 398:that proved crucial. 194: 183: 131: 2780:Auxiliary power unit 2188:Flight control modes 1790:Flight International 1778:Flight International 1538:. 4 September 2009. 1276:Crickmore, Paul F. " 1072:Launch escape system 1022:Buran-class orbiters 744:Early models of the 659:improve this section 311:Messerschmitt Bf 110 187:WY6AM ejection seat. 50:improve this article 2876:Romanian inventions 2759:Escape crew capsule 2666:War emergency power 2537:Pitot–static system 2382:Variable-sweep wing 2090:Vertical stabilizer 1799:"The Ejection Site" 1792:. 16 December 1965. 1780:. 14 November 1952. 1664:"The Ejection Site" 1586:"Ejection Tie Club" 1342:"Photo #: NH 90350" 735:B-52 Stratofortress 405:Seat on display at 162:escape crew capsule 2467:Attitude indicator 2447:Airspeed indicator 2442:Aircraft periscope 1833:"Ejection History" 1824:The Globe and Mail 1774:"Up, Out and Down" 1641:. 27 August 2012. 1016:were the only two 948:are equipped with 902: 848: 801: 727: 703: 552: 544: 464: 410: 407:RAF Museum Cosford 238:Paris-Orly Airport 207: 189: 134: 2848: 2847: 2775:Aircraft lavatory 2512:Heading indicator 2457:Annunciator panel 2437:Air data computer 2347:Leading-edge cuff 1769: 1768: 1348:. 16 April 2001. 1303:Popular Mechanics 1103:Explanatory notes 1092:Ejection Tie Club 1077:Airborne lifeboat 874:. On landing, an 786:F-35 Lightning II 754:center of gravity 746:F-104 Starfighter 723:Mountain Home AFB 717:aircraft with an 695: 694: 687: 586:Fairford Air Show 437:rocket propulsion 293:impulse jets for 230:Anastase Dragomir 126: 125: 118: 100: 2888: 2830:Navigation light 2810:Hydraulic system 2785:Bleed air system 2713:Drogue parachute 2387:Vortex generator 2005:Interplane strut 1912: 1905: 1898: 1889: 1888: 1884: 1882: 1880: 1874: 1864: 1852: 1847:. Archived from 1836: 1827: 1826:. July 23, 2010. 1815: 1802: 1793: 1781: 1758: 1757: 1741: 1740: 1732: 1704: 1703: 1685: 1679: 1678: 1676: 1675: 1660: 1654: 1653: 1651: 1650: 1635: 1629: 1628: 1626: 1619: 1611: 1605: 1604: 1602: 1601: 1582: 1576: 1575: 1573: 1572: 1557: 1551: 1550: 1548: 1547: 1526: 1520: 1519: 1514:. Archived from 1503: 1497: 1496: 1494: 1493: 1478: 1472: 1467: 1461: 1460: 1458: 1457: 1438: 1432: 1431: 1429: 1428: 1413: 1407: 1406: 1404: 1403: 1367: 1361: 1360: 1358: 1357: 1338: 1332: 1331: 1329: 1328: 1313: 1307: 1306: 1295: 1289: 1274: 1268: 1267: 1265: 1264: 1245: 1239: 1238: 1236: 1235: 1220: 1214: 1213: 1211: 1210: 1195: 1189: 1188: 1170: 1164: 1163: 1161: 1160: 1145: 1128: 1125: 1119: 1113: 1057:Caterpillar Club 1033:James Bond films 1029:Aston Martin DB5 690: 683: 679: 676: 670: 639: 631: 517:Fairchild Hiller 394:and his company 373:pusher propeller 369:the twin engines 215:Everard Calthrop 203:Crash test dummy 121: 114: 110: 107: 101: 99: 58: 34: 26: 2896: 2895: 2891: 2890: 2889: 2887: 2886: 2885: 2851: 2850: 2849: 2844: 2840:Ram air turbine 2805:Flight recorder 2763: 2742: 2675: 2656:Thrust reversal 2580: 2571: 2542:Radar altimeter 2507:Head-up display 2417: 2406: 2302:Anti-shock body 2284: 2272: 2133:Artificial feel 2115:Flight controls 2109: 1975:Fabric covering 1925: 1921:components and 1916: 1878: 1876: 1872: 1863:. 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Stennis 316:Heinkel He 219 295:V-1 flying bomb 234:parachuted cell 178: 122: 111: 105: 102: 65:"Ejection seat" 59: 57: 47: 35: 24: 17: 12: 11: 5: 2894: 2884: 2883: 2878: 2873: 2868: 2863: 2861:Ejection seats 2846: 2845: 2843: 2842: 2837: 2832: 2827: 2825:Landing lights 2822: 2817: 2812: 2807: 2802: 2797: 2792: 2787: 2782: 2777: 2771: 2769: 2765: 2764: 2762: 2761: 2756: 2750: 2748: 2747:Escape systems 2744: 2743: 2741: 2740: 2735: 2730: 2725: 2720: 2715: 2710: 2705: 2700: 2695: 2689: 2687: 2685:arresting gear 2677: 2676: 2674: 2673: 2668: 2663: 2658: 2653: 2648: 2643: 2641:Splitter plate 2638: 2633: 2628: 2623: 2618: 2613: 2608: 2603: 2598: 2593: 2587: 2585: 2573: 2572: 2570: 2569: 2564: 2559: 2554: 2549: 2544: 2539: 2534: 2529: 2524: 2519: 2514: 2509: 2504: 2499: 2494: 2489: 2484: 2479: 2474: 2469: 2464: 2459: 2454: 2449: 2444: 2439: 2434: 2429: 2423: 2421: 2408: 2407: 2405: 2404: 2399: 2394: 2389: 2384: 2379: 2374: 2369: 2364: 2359: 2354: 2349: 2344: 2339: 2334: 2329: 2324: 2319: 2314: 2309: 2304: 2299: 2294: 2288: 2286: 2274: 2273: 2271: 2270: 2265: 2260: 2255: 2250: 2245: 2240: 2235: 2230: 2225: 2220: 2215: 2210: 2205: 2200: 2195: 2190: 2185: 2180: 2175: 2170: 2165: 2160: 2155: 2150: 2145: 2140: 2135: 2130: 2125: 2119: 2117: 2111: 2110: 2108: 2107: 2102: 2097: 2092: 2087: 2082: 2077: 2072: 2067: 2062: 2057: 2052: 2047: 2042: 2037: 2032: 2027: 2022: 2017: 2012: 2007: 2002: 1997: 1992: 1987: 1982: 1977: 1972: 1967: 1962: 1960:Cruciform tail 1957: 1955:Crack arrestor 1952: 1947: 1942: 1936: 1934: 1927: 1926: 1915: 1914: 1907: 1900: 1892: 1886: 1885: 1865: 1853: 1851:on 2007-10-07. 1837: 1828: 1816: 1812:Authorsden.com 1803: 1794: 1782: 1767: 1766: 1751: 1750: 1746: 1745: 1744:External image 1738: 1737:External links 1735: 1734: 1733: 1720:Air Enthusiast 1712: 1709: 1706: 1705: 1698: 1680: 1655: 1630: 1627:on 2013-09-03. 1606: 1577: 1552: 1521: 1518:on 2014-09-23. 1512:Bharat Rakshak 1498: 1473: 1462: 1433: 1408: 1386:. p. 56. 1378:. 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2701: 2699: 2698:Arrestor hook 2696: 2694: 2693:Aircraft tire 2691: 2690: 2688: 2686: 2682: 2678: 2672: 2669: 2667: 2664: 2662: 2659: 2657: 2654: 2652: 2649: 2647: 2644: 2642: 2639: 2637: 2634: 2632: 2629: 2627: 2624: 2622: 2619: 2617: 2614: 2612: 2609: 2607: 2604: 2602: 2599: 2597: 2594: 2592: 2589: 2588: 2586: 2584: 2578: 2574: 2568: 2565: 2563: 2560: 2558: 2555: 2553: 2550: 2548: 2545: 2543: 2540: 2538: 2535: 2533: 2530: 2528: 2525: 2523: 2520: 2518: 2515: 2513: 2510: 2508: 2505: 2503: 2500: 2498: 2497:Glass cockpit 2495: 2493: 2490: 2488: 2485: 2483: 2480: 2478: 2475: 2473: 2470: 2468: 2465: 2463: 2460: 2458: 2455: 2453: 2450: 2448: 2445: 2443: 2440: 2438: 2435: 2433: 2432:Air data boom 2430: 2428: 2425: 2424: 2422: 2419: 2413: 2409: 2403: 2400: 2398: 2395: 2393: 2390: 2388: 2385: 2383: 2380: 2378: 2375: 2373: 2370: 2368: 2365: 2363: 2360: 2358: 2355: 2353: 2350: 2348: 2345: 2343: 2340: 2338: 2335: 2333: 2330: 2328: 2325: 2323: 2320: 2318: 2315: 2313: 2310: 2308: 2305: 2303: 2300: 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1862: 1861:Aviation Week 1858: 1854: 1850: 1846: 1842: 1838: 1834: 1829: 1825: 1821: 1817: 1813: 1809: 1804: 1800: 1795: 1791: 1787: 1783: 1779: 1775: 1771: 1770: 1765: 1764:Flight Global 1761: 1752: 1747: 1742: 1730: 1726: 1722: 1721: 1715: 1714: 1701: 1699:0-9633974-4-3 1695: 1691: 1684: 1669: 1665: 1659: 1644: 1640: 1634: 1623: 1616: 1610: 1595: 1591: 1587: 1581: 1566: 1562: 1556: 1541: 1537: 1536: 1531: 1525: 1517: 1513: 1509: 1502: 1487: 1483: 1477: 1471: 1466: 1451: 1447: 1443: 1437: 1422: 1418: 1412: 1397: 1393: 1389: 1385: 1381: 1377: 1373: 1366: 1351: 1347: 1343: 1337: 1322: 1318: 1312: 1304: 1300: 1294: 1287: 1286:1-880588-23-4 1283: 1279: 1273: 1258: 1254: 1250: 1244: 1229: 1225: 1219: 1204: 1200: 1194: 1186: 1184:0-88365-666-3 1180: 1176: 1169: 1155:on 2010-11-22 1154: 1150: 1144: 1140: 1124: 1118: 1112: 1108: 1093: 1090: 1088: 1087:Pressure suit 1085: 1083: 1080: 1078: 1075: 1073: 1070: 1068: 1065: 1063: 1060: 1058: 1055: 1052: 1049: 1048: 1041: 1036: 1034: 1030: 1025: 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Retrieved 1153:the original 1143: 1123: 1116: 1111: 1026: 1012: 1007: 994: 991: 976: 965: 954: 935: 922: 914: 903: 861: 852:B-58 Hustler 849: 845:B-58 Hustler 830: 819: 809: 802: 782:T-6 Texan II 762: 758: 743: 739:Crew Capsule 732: 728: 704: 681: 672: 657:Please help 645: 621: 617: 603: 594: 579: 568: 559: 553: 538: 533:A-4E Skyhawk 523:Pilot safety 505:Rogallo wing 500: 496: 489: 465: 458: 433: 417: 411: 396:Martin-Baker 392:James Martin 377: 364: 348: 340: 338: 323: 317: 304: 291:Argus As 014 268: 261: 257:World War II 254: 233: 227: 208: 185:Martin-Baker 166:B-58 Hustler 158:rocket motor 146:ejector seat 145: 141: 135: 112: 103: 93: 86: 79: 72: 60: 48:Please help 43:verification 40: 2738:Tundra tire 2621:Intake ramp 2552:Transponder 2337:Gurney flap 2278:Aerodynamic 2193:Fly-by-wire 2075:Triple tail 1841:"Mk10 seat" 938:Kamov Ka-50 839:Crewmember 805:shell tooth 429:flying wing 283:jet-engined 2855:Categories 2728:Oleo strut 2616:Inlet cone 2611:Gascolator 2577:Propulsion 2567:Yaw string 2562:Variometer 2418:instrument 2397:Wing fence 2332:Gouge flap 2307:Blown flap 2263:Yaw damper 2238:Stabilator 2223:Side-stick 2158:Dive brake 2045:Stabilizer 2020:Lift strut 2010:Jury strut 1674:2013-05-15 1649:2013-05-15 1600:2016-10-31 1571:2016-10-31 1546:2016-10-31 1492:2012-04-20 1456:2016-10-31 1446:NPP Zvezda 1427:2018-11-18 1402:2014-05-17 1392:B0019QSQ1E 1356:2016-10-31 1327:2012-10-30 1263:2012-10-30 1234:2012-10-30 1209:2012-10-30 1159:2012-10-30 1067:Escape pod 1013:Enterprise 985:, and the 942:helicopter 776:family of 606:Royal Navy 598:NPP Zvezda 575:chimpanzee 539:Shangri-La 511:design by 509:gyrocopter 476:D-21 drone 341:Volksjäger 281:prototype 219:parachutes 199:F-15 Eagle 76:newspapers 2703:Autobrake 2631:NACA duct 2606:Fuel tank 2596:Drop tank 2579:controls, 2462:Astrodome 2452:Altimeter 2317:Dog-tooth 2282:high-lift 2233:Spoileron 2218:Servo tab 2198:Gust lock 2153:Deceleron 2138:Autopilot 2095:Wing root 2080:Twin tail 2065:Tailplane 2000:Hardpoint 1970:Empennage 1933:structure 1729:0143-5450 1288:, page 90 1135:Citations 1031:from the 925:parachute 908:and zero 646:does not 537:USS  492:U.S. Navy 484:Mach 3.25 457:USS  250:Bucharest 170:parachute 152:or other 2871:Rocketry 2671:Wet wing 2646:Throttle 2392:Vortilon 2253:Trim tab 2183:Flaperon 2173:Elevator 2128:Airbrake 2100:Wing tip 2025:Longeron 1995:Fuselage 1931:Airframe 1919:Aircraft 1668:Archived 1643:Archived 1594:Archived 1565:Archived 1540:Archived 1486:Archived 1450:Archived 1421:Archived 1396:Archived 1350:Archived 1321:Archived 1257:Archived 1228:Archived 1203:Archived 1082:Lifeboat 1045:See also 1008:Columbia 995:Columbia 910:airspeed 906:altitude 767:and the 765:BAE Hawk 675:May 2013 472:Canberra 138:aircraft 106:May 2013 2681:Landing 2472:Compass 2420:systems 2412:Avionic 2402:Winglet 2285:devices 2228:Spoiler 2123:Aileron 2105:Wingbox 2030:Nacelle 1980:Fairing 1923:systems 1879:1 April 1224:"Moved" 1199:"Moved" 1149:"1910s" 917:impulse 868:capsule 843:from a 820:Soviet 769:Harrier 719:ACES II 667:removed 652:sources 455:aboard 357:shotgun 353:cockpit 334:Saab 17 330:Saab 21 286:fighter 271:Heinkel 248:, near 246:Băneasa 176:History 90:scholar 2416:flight 2377:Strake 2208:Rudder 2178:Elevon 2143:Canard 2085:V-tail 2060:T-tail 1990:Former 1950:Canopy 1727:  1696:  1390:  1284:  1253:Flight 1181:  1040:G-seat 983:Gemini 979:Vostok 946:rotors 895:MiG-29 876:airbag 750:T-tail 590:MiG-29 478:, two 388:spring 326:Bofors 264:forces 211:bungee 92:  85:  78:  71:  63:  2881:Seats 2601:FADEC 2487:EICAS 2362:Slats 2203:HOTAS 2055:Strut 1873:(PDF) 1625:(PDF) 1618:(PDF) 1098:Notes 1004:STS-4 1000:STS-1 899:Su-30 812:Lexan 573:with 365:Pfeil 349:Spatz 242:Paris 240:near 150:pilot 140:, an 97:JSTOR 83:books 2683:and 2547:TCAS 2527:ISIS 2482:EFIS 2427:ACAS 2414:and 2367:Slot 2327:Flap 2280:and 2268:Yoke 2040:Spar 1965:Dope 1881:2023 1725:ISSN 1694:ISBN 1388:ASIN 1282:ISBN 1179:ISBN 1010:and 966:The 936:The 891:K-36 854:and 822:VTOL 799:jets 784:and 778:VTOL 715:F-16 650:any 648:cite 303:the 275:SAAB 273:and 154:crew 69:news 2522:INS 2502:GPS 2357:LEX 2035:Rib 1762:by 1002:to 661:by 499:or 318:Uhu 144:or 136:In 52:by 2857:: 1859:. 1843:. 1822:. 1810:. 1788:. 1776:. 1666:. 1592:. 1588:. 1532:. 1510:. 1448:. 1444:. 1394:. 1374:. 1344:. 1301:. 1251:. 989:. 981:, 897:, 788:. 741:. 431:. 347:A 225:. 209:A 1911:e 1904:t 1897:v 1883:. 1835:. 1814:. 1801:. 1731:. 1702:. 1677:. 1652:. 1603:. 1574:. 1549:. 1495:. 1459:. 1430:. 1405:. 1359:. 1330:. 1266:. 1237:. 1212:. 1187:. 1162:. 688:) 682:( 677:) 673:( 669:. 655:. 560:g 556:g 462:. 262:g 205:. 119:) 113:( 108:) 104:( 94:· 87:· 80:· 73:· 46:. 23:.

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