535:
1117:
741:
to the variable-diameter tube with a wider rear section to provide the missile with better acceleration, and back to a straight tube to prevent its explosion due to a critical pressure drop or accidental booster detonation. Canards of the basic missile design were housed within the missile body during the entire flight, coming outside only to correct the course deviation of each roll cycle and folding back within a split second, variable incidence (instead of fixed) canards were used to improve terminal guidance accuracy. The seeker also changed drastically, with multiple modifications made during the test phase, the most important of which making it
427:, began examining a weapon that would fill both of these requirements. When initial studies proved promising, in January 1956 the company began an 11-month study which they named "Redeye" due to its infrared seeker. To lower prototype costs, the missile would initially be based on the unguided FFAR, which was already in widespread production. This would be turned into a missile by replacing the contact-fused warhead of the FFAR with a new seeker system and smaller 1.2-pound (0.54 kg) warhead. In production models, the motor would be modified to burn only briefly to propel it about 25 feet (8 m) at low speed before firing at full thrust.
691:
749:,) and reducing the field of view to increase the missile's capability against single engine jets. Among the design improvements made in the seeker gyro were an increased aperture to provide greater sensitivity; a new center post design for supporting the secondary mirror to improve background discrimination; a new gyro gimbal of increased rigidity; an improved lead sulfide cell, doubling its sensitivity; and an improved reticle with a reduced field of view. Unorthodox designs included the "Foxhole Redeye," which was small enough to be stored and fired from a rifleman's
705:
719:
1103:
31:
661:
launches the missile out of the tube at a speed of around 80 feet per second (25 m/s). As the missile leaves the tube, spring-loaded fins pop out—four stabilizing tail fins at the back of the missile, and two control surfaces at the front of the missile. Once the missile has traveled six meters, the sustainer motor ignites. The sustainer motor takes the missile to its peak velocity of Mach 1.7 in 5.8 seconds. The warhead is armed 1.2 seconds after the sustainer is ignited.
558:
1313:
1235:
1170:
495:, adapted for ground use and scaled-down to be operated by hand and launched from a disposable tube. The lead that Convair had over these weapons was unapproachable, and their proposal was strongly supported by the Marines, who pressed the Army to begin development. They also suggested that the system would suffer from a number of issues during development related to the airframe and seeker, but felt that these were not enough to hold up development.
1287:
1222:
1144:
1248:
1157:
1300:
1209:
1196:
1183:
1079:
1261:
1326:
1131:
1274:
395:(FFARs) at an effective rate of 6,000 rounds per minute. The system was never built in complete form, and cancelled in February 1956. Octopus, from 1953, re-examined the .50 and .60 rounds, as well as the emerging 20 mm round based on the latter. This project also failed to deliver an operational system.
625:
All Redeye missiles were numbered and inventorized by the US Army
Missile Command to prevent them from disappearance or otherwise unnoticed losses. No Redeye missiles were reported lost or stolen from the Army inventory, but losses occurred after Redeyes were supplied to foreign troops. This happened
740:
of their optics, and were either separable or non-separable, which in turn could be built-in or molded-in primitive mechanical sight with flashing diodes inside diopter to inform gunner of seeker's lock-on. The launch tube changed its design and shape several times, from pipelike straight-shaped one
731:
During its development, the weapon underwent several major design changes. Initially, its gripstock was literally just a gripstock with grips, stock and trigger only, later evolved in a separable launch unit with optics, electronics, and battery input. Several designs had no optical sighting device;
328:
program. It was initially banned from being sold overseas, to avoid missiles falling into the hands of terrorist organizations. However, after the export ban was lifted, the weapon was never actually used by terrorists against civil aircraft, in contrast with other MANPADS. While the Redeye and 9K32
660:
and then the operator begins to visually track the target using the sight unit on the launcher. Once the target is locked onto by the missile, a buzzer in the launcher hand grip begins vibrating, alerting the operator. The operator then presses the trigger, which fires the initial booster stage and
551:
resolved (eventually leading to the
Stinger development). Consequently, several other unsolicited proposals competed with the Redeye in the early 1960s. These included both guided (engaging target using techniques other than infrared homing) and unguided (directionally-controlled) missile systems.
550:
Deficiencies and shortcomings were experienced during the system development phase—mainly seeker inability to discriminate target against cloudy background or in a heavy clutter environment, coupled with absence of night operation capability and inability to engage head-on targets—which were never
406:
were now expected to fly at low altitudes. This led to a 1954 requirement for a lightweight system able to engage targets from 0 to 1,000 ft (300 m), and larger weapons that raised the ceiling to 10,000 ft (3,000 m). In order to improve its capability in poor visibility, it was
506:
The original design consisted of a simple tube with a clip-on grip system. The operator would simply point the tube in the general direction of the target, and fire when he heard the seeker make its "growl" sound, indicating it was locked onto the target. In May 1958 six unguided launches were
390:
in London, the US, UK and France agreed that the M2 would remain effective up until about 1960, but new weapons would be needed after that time. This led to development of the
Porcupine and Octopus concepts in the US. Porcupine, started in 1951, was a 64-barrel rocket launcher firing salvos of
542:
In July 1959 the development project began, in March 1960, the advanced test rounds were fired. Launches from a launch tube followed in May 1961, with a shoulder launch occurring in 1961. Technical problems prevented the missile entering full production: The missile did not live up to its
434:
in
November 1956. Simulations suggested that it would have an average miss distance of 4 to 8 feet (1.2 to 2.4 m), and a direct-hit probability of 0.35 to 0.40. The design proved extremely interesting, and in 1957 official requirements were formulated. This led to the Army's
565:
Block II systems designated XM41E1 began development in 1964, the missile being designated XMIM-43B. The missiles were delivered in April 1966, and included a new gas-cooled infrared detector cell, a slightly redesigned launcher and an improved warhead.
358:
would not be capable against future high-performance aircraft. They published a new requirement for a weapon suitable for engagements between 25 and 2,500 yards (23 and 2,300 m) against targets flying up to 1,000 miles per hour (1,600 km/h).
664:
The missile's seeker is capable only of acquiring and tracking the hot exhaust of aircraft, which limits the engagements to tail-chase only, tracking the rapidly receding target. The missile's blast fragmentation warhead is triggered by an impact
346:
weapons. They called for the development of new weapons that would be the best in the world, while also being able to be separated into loads of no more than 25 pounds (11 kg). When considering anti-aircraft weapons, they concluded that the
324:) after about 85,000 rounds had been built. The Redeye was withdrawn gradually between 1982 and 1995 as the Stinger was deployed, though it remained in service with various armed forces of the world until quite recently, being supplied via the
578:. The missile achieved a kill probability against F9F tactical drones travelling at 490 mph (800 km/h) at an altitude of 330 ft (100 m) of 0.51. From this it was calculated that the kill probability versus a
569:
In 1965 to 1966 General
Dynamics developed the final Redeye Block III configuration, designated at first XM41E2 with XFIM-43C missiles. The missiles retained the seeker from the Block II missile, but included a new
487:(Col. James E. Linka, a supervising officer with OCRD Air Defense and Missiles Division, responsible for Stinger, later recalled that Lockheed entered the competition in 1959, but no details were ever disclosed.)
2097:
2186:
757:
units. All interim designs were dropped in favor of the one which was considered the best possible choice by the Army
Missile Command, and mass-produced at the General Dynamics facilities within the
3146:
374:
system. Development on this system continued until 1951, when the requirement was extended to 14,000 feet (4,300 m), which could not be met by the 0.60 round. A new concept using a
3225:
2076:
3423:
3428:
2089:
523:
of the new weapon, as well as a trooper's capability to aim and launch a missile from the shoulder safely and accurately towards an imaginary target. In June 1958 the
3185:
366:
Ordnance Corps began development of the "Stinger" system, essentially an updated version of the
Quadmount mounting four T17 machine guns firing the more powerful
329:
Strela-2 (SA-7) were similar, the missiles were not identical. Nonetheless, the CIA concluded that the Soviet SA-7 had benefited from the Redeye's development.
508:
554:
Limited production began as XM41 Redeye Block I. The missile was designated XMIM-43A in June 1963. Block I systems were then evaluated between 1965 and 1966.
753:, and the "unitized launcher Redeye" fire-and-discard variant as a fully discardable throw-away unit with no separable elements for use with the USMC and
3433:
2828:
2796:
732:
the gunner was supposed to rely on the auditory alarm when the seeker acquired the target. Those with optical sights differed one from another in shape,
1376:
2052:
3023:
3018:
2903:
2858:
3292:
3195:
3156:
2988:
2823:
1763:
538:
MICOM Commander
General John G. Zierdt inspecting interim Redeye production model, disposable variant (note the optics and launcher design)
543:
specifications, being slower, less maneuverable and less accurate. During the testing, substantial use was made of the
Atlantic Research
2124:
1652:
REDEYE II SOLE SOURCE PROCUREMENT, Statement of Lt. Col. James E. Linka, Office, Chief
Research and Development, Department of the Army
1736:
3170:
2993:
2755:
1703:
3337:
2750:
761:. The following is the list, featuring the basic model, designated FIM-43A and approved for production along with its derivatives:
2816:
1545:
626:
first in Belgium in January 1974, causing a strengthening of security measures in the major West European and British airports.
448:, a crew-served partially portable surface-to-air missile system, designed by the Drone and Missile Flight Control Departmentof
498:
On 14 April 1958, the development contract was released and Convair was awarded a contract to start development of the system.
3372:
3342:
3126:
2177:
102:
574:, warhead and fuze. The launcher now had an XM-62 open sight and upgraded electronics. The new missile could turn at up to 3
316:
to track its target. Production began in 1962 and – in anticipation of the Redeye II, which later became the
2661:
590:
was estimated at 0.43. Production of the Block III systems began in May 1967. In 1968 Block III was declared operational.
3377:
3251:
1950:
480:
677:
and hot brick jammers. Its inability to turn at a rate greater than 3g means that it can be outmaneuvered, if detected.
2036:
1122:
1984:
2155:
3297:
3141:
2853:
1651:
1353:
512:
306:
745:, increasing its discrimination capability (though extending reaction time in order to adjust its subsystems to
3332:
774:/XFIM-43B/XMIM-43B – Fitted with a gas cooled seeker and improved warhead and fuse and modified launcher.
387:
3402:
3054:
3039:
1524:
534:
1791:
1779:
3395:
3322:
3317:
3136:
3003:
2056:
520:
1953:
S.A.M. use in current terrorist operations. Jack Urso for Military Information Services, December 31, 2003
2801:
1803:
637:
320: – ended in the early 1970s (delivery of the last Redeye for the US Army was completed in
1900:
1496:
464:(Shoulder-Launched Antiaircraft Missile), a man-portable surface-to-air missile system, designed by the
3312:
3096:
2776:
2541:
2536:
2415:
1962:
431:
2963:
2878:
2811:
2641:
2405:
2170:
1348:
3352:
3287:
758:
528:
392:
2791:
579:
469:
1760:
2606:
1512:
674:
618:
helicopters. By November 1986 it had largely been replaced by the dramatically more successful
399:
325:
309:
3438:
3161:
2953:
2526:
2430:
2133:
954:
746:
657:
645:
603:
484:
453:
94:
90:
788:/XFIM-43C – Production version; improved warhead and fuse section, and a new launcher.
690:
3357:
3307:
3215:
2725:
2163:
1808:
1740:
106:
1475:
586:
and US H-13 and H-21). Kill probability against larger propeller driven aircraft like the
8:
2863:
2703:
2626:
1712:
704:
492:
1938:
1446:
Merged with other subdivisions to form Sperry Surface Armament Division later that year.
2938:
2888:
2745:
2713:
2420:
2278:
750:
718:
473:
363:
98:
1420:
3367:
3347:
2998:
2943:
2898:
2868:
2666:
2656:
2491:
2236:
2185:
2150:
2032:
1980:
1687:
1483:
666:
656:
The missile is fired from the M171 missile launcher. First, the seeker is cooled to
342:
In May 1946, the War Department Equipment Board published a report on the future of
3362:
3267:
2983:
2968:
2848:
2843:
2735:
2596:
2586:
2360:
2350:
2333:
2248:
1343:
599:
582:
at similar altitude would be 0.403, and 0.53 against helicopters (specifically the
544:
449:
436:
424:
299:
143:
439:
receiving several unsolicited proposals for similar weapons from other companies:
3220:
3205:
3175:
3116:
3064:
3059:
3013:
2928:
2883:
2786:
2631:
2601:
2571:
2566:
2561:
2410:
2395:
2390:
2365:
2355:
2328:
2293:
2258:
2226:
2211:
1767:
408:
403:
378:
firing a new 37 mm round emerged, but proved too complex and was cancelled.
375:
313:
290:
1688:
Redstone Arsenal Historical Information: Redeye Background and System Chronology
3282:
3180:
3106:
3079:
3008:
2873:
2781:
2740:
2708:
2693:
2651:
2546:
2521:
2506:
2470:
2460:
2425:
2400:
2380:
2345:
2298:
2263:
2221:
1690:, U.S. Army Aviation and Missile Command Official Web-site. Verified 05.12.2017
1396:
670:
619:
317:
30:
3417:
3121:
3086:
3074:
3069:
2958:
2806:
2616:
2556:
2531:
2511:
2501:
2475:
2455:
2450:
2445:
2440:
2340:
2323:
2273:
2253:
2231:
2206:
2201:
1381:
1318:
824:
817:
737:
733:
669:, requiring a direct hit. As a first-generation missile it is susceptible to
587:
571:
557:
348:
3246:
3230:
3210:
3200:
3190:
3151:
3101:
3091:
3044:
2978:
2948:
2908:
2893:
2730:
2683:
2636:
2611:
2576:
2496:
2385:
2303:
2216:
1331:
1240:
607:
2918:
2688:
2678:
2581:
2369:
2318:
2288:
2283:
2268:
2243:
1175:
524:
402:(SAMs) were rendering higher altitude flight increasingly dangerous, and
355:
352:
86:
2720:
2621:
2591:
963:
606:
in 1984, where they were used to shoot down aircraft including several
516:
465:
3302:
2516:
2465:
1963:
General Dynamics FIM-43 Redeye Man-Portable Air Defense System (1968)
1108:
644:" to shoot down at least four Soviet Mil Mi-8 helicopters during the
611:
321:
2077:
The Central African Republic:A CASE STUDY OF SMALL ARMS AND CONFLICT
3165:
1408:
1292:
1227:
1078:
615:
583:
343:
110:
3049:
2923:
2913:
2838:
2771:
1941:
Christopher Chant - Aviation and military history, April 15, 2013
1358:
1253:
1162:
1149:
742:
641:
575:
420:
125:
1711:. Historical Division Army Missile Command. 1974. Archived from
430:
The resulting concept mockups were demonstrated to the Army and
3131:
3111:
2973:
2933:
2833:
2698:
2673:
2646:
2551:
1305:
1279:
1214:
1201:
1188:
754:
2045:
266:
First stage – Booster (Ejector): 3.3 kN (750 lbf) for 0.048 s
3327:
3277:
3272:
2375:
2313:
2308:
2132:. Redstone Arsenal, U.S. Army Missile Command. Archived from
1525:
STINGER: Redeye Missile Replacement Being Developed for 1980s
1266:
371:
1932:
1929:
The small secondary charge ignites any remaining propellent
1364:
1136:
561:
The block I/II launcher above, the block III launcher below
367:
273:
794: – Experimental missile, with data logging capability
780: – Experimental missile, with data logging capability
944:
936:
930:
2031:(5 ed.). Jane's Information Group. pp. 56–57.
1113:
3397:
United States tri-service rocket designations post-1963
1761:
Sukhoi Su-25 Frogfoot: Described / SU-25 In Afghanistan
1513:
Fiscal Year 1973 Authorization for Military Procurement
1476:
https://twitter.com/war_noir/status/1701072142903767080
1633:
3424:
Cold War surface-to-air missiles of the United States
1824:
1822:
2151:
General Dynamics FIM-43 Redeye - Designation Systems
1611:
1609:
1596:
1594:
1569:
1567:
802: – Upgraded missile, with unknown capabilities.
633:
in Danish service and as RBS 69 in Swedish service.
268:
Second stage – Sustainer: 1.1 kN (250 lbf) for 5.8 s
2187:
1963 United States Tri-Service missile designations
1669:
1657:
1425:
1413:
1401:
1389:
1377:List of U.S. Army rocket launchers by model number
3429:Naval surface-to-air missiles of the United States
1819:
1621:
1792:Hearings on thefts and losses of military weapons
1780:Hearings on thefts and losses of military weapons
1606:
1591:
1579:
1564:
1552:
1546:"Meet the Missile That Started the MANPADS Craze"
3415:
2022:
2020:
2018:
2016:
2014:
2012:
2010:
2008:
2006:
2004:
2002:
2000:
1998:
1996:
1654:, Hearings on S. 3108, March 10, 1972, p. 3701.
491:The competing designs were based on various US
398:By the mid-1950s, new medium and high-altitude
2090:"Sandinistas report capture of RedEye Missile"
940:and 0.71 oz (20 g) secondary charge
2171:
1939:The Redeye – A pioneering battlefield missile
1993:
1064:100 to 10,000 ft (0.03 to 3.0 km)
640:by the US were also used by the Nicaraguan "
1067:160 to 8,900 ft (0.05 to 2.7 km)
1061:160 to 7,500 ft (0.05 to 2.3 km)
598:Fifty Redeye systems were delivered to the
3434:Military equipment introduced in the 1960s
2178:
2164:
2026:
1698:
1696:
1470:
1468:
2027:Cullen, Tony; Foss, C.F. (1 March 1992).
407:suggested that the weapon be aimed using
1077:
556:
533:
381:
337:
1979:(first ed.). Osprey. p. 222.
1693:
1508:
1506:
1465:
1082:Map with former FIM-43 operators in red
1050:690 mph (310 m/s) (receding)
1047:580 mph (260 m/s) (receding)
969:Tail-chase / limited forward-hemisphere
3416:
2087:
971:(depending on conditions and version)
2159:
2122:
2029:Jane's Land-based Air Defence 1992-93
1974:
1675:
1663:
1639:
1627:
1615:
1600:
1585:
1573:
1558:
1503:
2126:History of the Redeye Weapon System
1705:History of the Redeye Weapon System
1086:
990:(2–4.3 μm sensitivity range).
983:(1–2.8 μm sensitivity range).
806:
44:Man-portable surface-to-air missile
16:Man-portable surface-to-air missile
13:
710:Foxhole variant being field-tested
14:
3450:
3403:Drones designated in UAV sequence
2144:
1965:Militaryfactory.com, July 7, 2015
529:feasibility demonstration program
481:Lockheed Missile Systems Division
414:
2116:
2088:Kinzer, Stephen (23 July 1987).
1354:Coordination of Azawad Movements
1324:
1311:
1298:
1285:
1272:
1259:
1246:
1233:
1220:
1207:
1194:
1181:
1168:
1155:
1142:
1129:
1115:
1101:
724:FIM-43C Redeye just after launch
717:
703:
689:
636:Redeye missiles provided to the
602:by the United States during the
370:round and aimed by an automated
222:Effective firing range
29:
2812:BGM-109/AGM-109/RGM-109/UGM-109
2081:
2070:
1968:
1956:
1944:
1923:
1914:
1894:
1885:
1876:
1867:
1858:
1849:
1840:
1831:
1797:
1785:
1773:
1754:
1737:"SIPRI Arms Transfers Database"
1729:
1681:
1645:
1440:
509:Twentynine Palms proving ground
2123:Cagle, Mary T. (23 May 1974).
1901:‘Redeye’ Development Continued
1538:
1518:
1039:1,300 mph (580 m/s)
1036:1,000 mph (450 m/s)
1033:1,100 mph (500 m/s)
1025:14,800 ft (4,500 m)
1022:13,500 ft (4,100 m)
1019:13,800 ft (4,200 m)
651:
362:In response, in June 1948 the
332:
180:Specifications (FIM-43 Redeye)
158:
75:
1:
1529:Army Research and Development
1453:
1458:
1073:
1053:500 mph (225 m/s)
1008:FM-modulated (conical scan)
943:0.79 lb (0.36 kg)
935:0.82 lb (0.37 kg)
929:0.82 lb (0.37 kg)
521:human factors and ergonomics
7:
1370:
921:Blast fragmentation (M222)
903:2.3 lb (1.06 kg)
900:2.6 lb (1.17 kg)
897:2.6 lb (1.17 kg)
696:One of the earliest designs
680:
547:expendable target missile.
507:conducted by US Marines at
10:
3455:
960:Limited forward hemisphere
951:Missile engagement aspect
926:Warhead explosive content
872:23 lb (10.3 kg)
861:29 lb (13.3 kg)
593:
501:
479:an undesignated system by
3386:
3260:
3239:
3032:
2764:
2484:
2194:
1531:, October–November 1972,
1337:
1094:
1005:AM-modulated (spin scan)
889:55 in (1.40 m)
886:58 in (1.47 m)
883:57 in (1.44 m)
875:18 lb (8.3 kg)
869:22 lb (9.8 kg)
393:Folding Fin Arial Rockets
282:
272:
262:
257:
245:
237:
229:
221:
216:
208:
200:
192:
184:
179:
168:
157:
149:
139:
131:
121:
116:
82:
69:
61:
56:
49:Place of origin
48:
40:
28:
21:
1977:A Dictionary of Aviation
1975:Wragg, David W. (1973).
1837:Cagle, 1975, pp. 39, 62.
1433:
858:35 lb (16 kg)
855:33 lb (15 kg)
759:Greater Los Angeles Area
629:The Redeye was known as
423:, recently purchased by
391:2.75-inch (7.0 cm)
312:system. It uses passive
233:M222 Blast-fragmentation
1794:, November 1975, p. 57.
1782:, November 1975, p. 74.
580:Mikoyan-Gurevich MiG-21
470:North American Aviation
1123:Bosnia and Herzegovina
1083:
562:
539:
400:surface-to-air missile
326:Foreign Military Sales
310:surface-to-air missile
3373:M30 GMLRS/M31 GMLRS-U
1804:For SA-7 read Redeye?
1081:
1044:Maximum target speed
997:PbS detector element
747:operating temperature
658:operating temperature
646:Nicaraguan Revolution
560:
537:
485:Sunnyvale, California
454:Garden City, New York
388:Tripartite Conference
382:Porcupine and Octopus
338:Post-war developments
196:1.20 m (3 ft 11.5 in)
95:Nicaraguan Revolution
2657:AGM-84/RGM-84/UGM-84
2139:on 22 February 2004.
1809:Flight International
1058:Engagement altitude
993:Gas-cooled (FIM-43A:
988:PbS detector element
981:PbS detector element
918:blast fragmentation
913:blast fragmentation
107:Salvadoran Civil War
1920:Cagle, 1975, p. 71.
1891:Cagle, 1975, p. 62.
1882:Cagle, 1975, p. 39.
1873:Cagle, 1975, p. 36.
1864:Cagle, 1975, p. 85.
1855:Cagle, 1975, p. 63.
1846:Cagle, 1975, p. 41.
1828:Cagle, 1975, p. 69.
1812:, 17 January 1974,
493:air-to-air missiles
466:Autonetics Division
238:Warhead weight
225:4,500 m (14,800 ft)
35:Inert FIM-43 Redeye
1770:airtoaircombat.com
1766:2007-02-03 at the
1084:
1002:Seeker modulation
768:/XFIM-43A/XMIM-43A
563:
540:
474:Downey, California
364:United States Army
278:Mach 1.7 (580 m/s)
117:Production history
103:War in Afghanistan
99:Lebanese Civil War
3411:
3410:
1642:, pp. 15–17.
1491:Missing or empty
1344:Afghan Mujahideen
1071:
1070:
821:(missile: 9M32M)
786:Block III FIM-43C
610:jets, as well as
604:Soviet–Afghan War
296:
295:
241:1.06 kg (2.35 lb)
91:Soviet–Afghan War
3446:
3398:
2180:
2173:
2166:
2157:
2156:
2140:
2138:
2131:
2110:
2109:
2107:
2105:
2100:on March 8, 2016
2096:. Archived from
2085:
2079:
2074:
2068:
2067:
2065:
2064:
2055:. Archived from
2049:
2043:
2042:
2024:
1991:
1990:
1972:
1966:
1960:
1954:
1948:
1942:
1936:
1930:
1927:
1921:
1918:
1912:
1898:
1892:
1889:
1883:
1880:
1874:
1871:
1865:
1862:
1856:
1853:
1847:
1844:
1838:
1835:
1829:
1826:
1817:
1801:
1795:
1789:
1783:
1777:
1771:
1758:
1752:
1751:
1749:
1748:
1739:. Archived from
1733:
1727:
1726:
1724:
1723:
1717:
1710:
1700:
1691:
1685:
1679:
1673:
1667:
1661:
1655:
1649:
1643:
1637:
1631:
1625:
1619:
1613:
1604:
1598:
1589:
1583:
1577:
1571:
1562:
1556:
1550:
1549:
1548:. 29 March 2015.
1542:
1536:
1522:
1516:
1510:
1501:
1500:
1494:
1489:
1487:
1479:
1472:
1447:
1444:
1429:
1427:
1417:
1415:
1405:
1403:
1393:
1391:
1330:
1328:
1327:
1317:
1315:
1314:
1304:
1302:
1301:
1291:
1289:
1288:
1278:
1276:
1275:
1265:
1263:
1262:
1252:
1250:
1249:
1239:
1237:
1236:
1226:
1224:
1223:
1213:
1211:
1210:
1200:
1198:
1197:
1187:
1185:
1184:
1174:
1172:
1171:
1161:
1159:
1158:
1148:
1146:
1145:
1135:
1133:
1132:
1125:
1121:
1119:
1118:
1107:
1105:
1104:
1087:Former operators
850:Weight of system
828:(missile: 9M36)
811:
810:
807:Comparison chart
772:Block II FIM-43B
721:
707:
693:
545:MQR-16 Gunrunner
463:
462:
450:Sperry Gyroscope
447:
446:
437:Redstone Arsenal
425:General Dynamics
300:General Dynamics
275:
188:8.3 kg (18.3 lb)
160:
144:General Dynamics
33:
24:
19:
18:
3454:
3453:
3449:
3448:
3447:
3445:
3444:
3443:
3414:
3413:
3412:
3407:
3396:
3382:
3256:
3235:
3028:
2899:RUM-125/UUM-125
2879:CQM-121/CGM-121
2760:
2480:
2190:
2184:
2147:
2136:
2129:
2119:
2114:
2113:
2103:
2101:
2086:
2082:
2075:
2071:
2062:
2060:
2051:
2050:
2046:
2039:
2025:
1994:
1987:
1973:
1969:
1961:
1957:
1949:
1945:
1937:
1933:
1928:
1924:
1919:
1915:
1905:Military Review
1899:
1895:
1890:
1886:
1881:
1877:
1872:
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1850:
1845:
1841:
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1827:
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1798:
1790:
1786:
1778:
1774:
1768:Wayback Machine
1759:
1755:
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1744:
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1247:
1245:
1234:
1232:
1221:
1219:
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1206:
1195:
1193:
1182:
1180:
1169:
1167:
1156:
1154:
1143:
1141:
1130:
1128:
1116:
1114:
1102:
1100:
1097:
1089:
1076:
996:
995:Peltier cooled)
994:
989:
987:
986:Nitrogen-cooled
982:
980:
970:
961:
939:
917:
916:Directed-energy
912:
911:Directed-energy
894:Warhead weight
866:Missile weight
852:ready to shoot
851:
831:FIM-43C Redeye
827:
820:
818:9K32M Strela-2M
809:
729:
728:
727:
726:
725:
722:
713:
712:
711:
708:
699:
698:
697:
694:
683:
671:countermeasures
654:
596:
504:
460:
459:
444:
443:
417:
409:infrared homing
404:attack aircraft
384:
376:revolver cannon
340:
335:
314:infrared homing
291:Infrared homing
287:
285:
267:
258:
250:
248:
217:
204:70 mm (2.75 in)
109:
105:
101:
97:
93:
89:
62:In service
57:Service history
36:
22:
17:
12:
11:
5:
3452:
3442:
3441:
3436:
3431:
3426:
3409:
3408:
3406:
3405:
3400:
3393:
3387:
3384:
3383:
3381:
3380:
3375:
3370:
3365:
3360:
3355:
3350:
3345:
3340:
3335:
3330:
3325:
3320:
3315:
3310:
3305:
3300:
3295:
3290:
3285:
3283:Common Missile
3280:
3275:
3270:
3264:
3262:
3258:
3257:
3255:
3254:
3249:
3243:
3241:
3237:
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3228:
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3213:
3208:
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3168:
3159:
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3119:
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3016:
3011:
3006:
3001:
2996:
2991:
2986:
2981:
2976:
2971:
2966:
2961:
2956:
2951:
2946:
2941:
2936:
2931:
2926:
2921:
2916:
2911:
2906:
2901:
2896:
2891:
2886:
2881:
2876:
2871:
2866:
2861:
2856:
2851:
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2841:
2836:
2831:
2826:
2821:
2820:
2819:
2809:
2804:
2799:
2794:
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2779:
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2762:
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2326:
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2306:
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2296:
2291:
2286:
2281:
2276:
2271:
2266:
2261:
2256:
2251:
2246:
2241:
2240:
2239:
2229:
2224:
2219:
2214:
2209:
2204:
2198:
2196:
2192:
2191:
2189:, 1963–present
2183:
2182:
2175:
2168:
2160:
2154:
2153:
2146:
2145:External links
2143:
2142:
2141:
2118:
2115:
2112:
2111:
2094:New York Times
2080:
2069:
2044:
2038:978-0710609793
2037:
1992:
1985:
1967:
1955:
1943:
1931:
1922:
1913:
1893:
1884:
1875:
1866:
1857:
1848:
1839:
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1818:
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1059:
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1041:
1040:
1037:
1034:
1031:
1030:Missile speed
1027:
1026:
1023:
1020:
1017:
1016:Maximum range
1013:
1012:
1009:
1006:
1003:
999:
998:
991:
984:
977:
973:
972:
967:
958:
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870:
867:
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862:
859:
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843:
840:
837:
836:Service entry
833:
832:
829:
822:
815:
808:
805:
804:
803:
797:
796:
795:
783:
782:
781:
769:
766:Block I FIM-43
723:
716:
715:
714:
709:
702:
701:
700:
695:
688:
687:
686:
685:
684:
682:
679:
653:
650:
620:FIM-92 Stinger
595:
592:
513:Camp Pendleton
503:
500:
489:
488:
477:
457:
416:
415:Redeye emerges
413:
383:
380:
351:mounting four
339:
336:
334:
331:
318:FIM-92 Stinger
294:
293:
288:
283:
280:
279:
276:
274:Maximum speed
270:
269:
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66:
63:
59:
58:
54:
53:
50:
46:
45:
42:
38:
37:
34:
26:
25:
23:FIM-43 Redeye
15:
9:
6:
4:
3:
2:
3451:
3440:
3437:
3435:
3432:
3430:
3427:
3425:
3422:
3421:
3419:
3404:
3401:
3399:
3394:
3392:
3389:
3388:
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3007:
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2605:
2603:
2600:
2598:
2595:
2593:
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2588:
2585:
2583:
2580:
2578:
2575:
2573:
2570:
2568:
2565:
2563:
2560:
2558:
2555:
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2535:
2533:
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2528:
2525:
2523:
2520:
2518:
2515:
2513:
2510:
2508:
2505:
2503:
2500:
2498:
2495:
2493:
2490:
2489:
2487:
2483:
2477:
2474:
2472:
2469:
2467:
2464:
2462:
2459:
2457:
2454:
2452:
2449:
2447:
2444:
2442:
2439:
2437:
2434:
2432:
2429:
2427:
2424:
2422:
2419:
2417:
2414:
2412:
2409:
2407:
2404:
2402:
2399:
2397:
2394:
2392:
2389:
2387:
2384:
2382:
2379:
2377:
2374:
2371:
2367:
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2357:
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2327:
2325:
2322:
2320:
2317:
2315:
2312:
2310:
2307:
2305:
2302:
2300:
2297:
2295:
2292:
2290:
2287:
2285:
2282:
2280:
2277:
2275:
2272:
2270:
2269:CGM-13/MGM-13
2267:
2265:
2262:
2260:
2257:
2255:
2252:
2250:
2247:
2245:
2242:
2238:
2235:
2234:
2233:
2230:
2228:
2225:
2223:
2220:
2218:
2215:
2213:
2210:
2208:
2205:
2203:
2200:
2199:
2197:
2193:
2188:
2181:
2176:
2174:
2169:
2167:
2162:
2161:
2158:
2152:
2149:
2148:
2135:
2128:
2127:
2121:
2120:
2117:Sources cited
2099:
2095:
2091:
2084:
2078:
2073:
2059:on 2014-09-03
2058:
2054:
2048:
2040:
2034:
2030:
2023:
2021:
2019:
2017:
2015:
2013:
2011:
2009:
2007:
2005:
2003:
2001:
1999:
1997:
1988:
1986:9780850451634
1982:
1978:
1971:
1964:
1959:
1952:
1951:FIM-43 REDEYE
1947:
1940:
1935:
1926:
1917:
1910:
1906:
1902:
1897:
1888:
1879:
1870:
1861:
1852:
1843:
1834:
1825:
1823:
1815:
1811:
1810:
1805:
1800:
1793:
1788:
1781:
1776:
1769:
1765:
1762:
1757:
1743:on 2009-08-05
1742:
1738:
1732:
1718:on 2016-03-29
1714:
1707:
1706:
1699:
1697:
1689:
1684:
1678:, p. 17.
1677:
1672:
1666:, p. 16.
1665:
1660:
1653:
1648:
1641:
1636:
1629:
1624:
1617:
1612:
1610:
1602:
1597:
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1575:
1570:
1568:
1560:
1555:
1547:
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1526:
1521:
1514:
1509:
1507:
1498:
1485:
1477:
1471:
1469:
1464:
1443:
1439:
1422:
1419:
1410:
1407:
1398:
1395:
1386:
1385:
1380:
1378:
1375:
1374:
1366:
1363:
1360:
1357:
1355:
1352:
1350:
1347:
1345:
1342:
1341:
1333:
1322:
1320:
1319:United States
1309:
1307:
1296:
1294:
1283:
1281:
1270:
1268:
1257:
1255:
1244:
1242:
1231:
1229:
1218:
1216:
1205:
1203:
1192:
1190:
1179:
1177:
1166:
1164:
1153:
1151:
1140:
1138:
1127:
1124:
1112:
1110:
1099:
1098:
1092:
1080:
1066:
1063:
1060:
1057:
1056:
1052:
1049:
1046:
1043:
1042:
1038:
1035:
1032:
1029:
1028:
1024:
1021:
1018:
1015:
1014:
1011:AM-modulated
1010:
1007:
1004:
1001:
1000:
992:
985:
978:
975:
974:
968:
966:) capability
965:
959:
956:
953:
950:
949:
946:
942:
938:
934:
932:
928:
925:
924:
920:
915:
910:
908:Warhead type
907:
906:
902:
899:
896:
893:
892:
888:
885:
882:
879:
878:
874:
871:
868:
865:
864:
860:
857:
854:
849:
848:
844:
841:
838:
835:
834:
830:
826:
825:9K34 Strela-3
823:
819:
816:
813:
812:
801:
798:
793:
790:
789:
787:
784:
779:
776:
775:
773:
770:
767:
764:
763:
762:
760:
756:
752:
748:
744:
739:
738:magnification
735:
734:field of view
720:
706:
692:
678:
676:
672:
668:
662:
659:
649:
647:
643:
639:
634:
632:
627:
623:
621:
617:
613:
609:
605:
601:
591:
589:
588:Antonov An-12
585:
581:
577:
573:
567:
559:
555:
552:
548:
546:
536:
532:
530:
527:phase of the
526:
522:
518:
514:
510:
499:
496:
494:
486:
482:
478:
475:
471:
467:
458:
455:
451:
442:
441:
440:
438:
433:
428:
426:
422:
412:
410:
405:
401:
396:
394:
389:
379:
377:
373:
369:
365:
360:
357:
354:
350:
349:M45 Quadmount
345:
330:
327:
323:
319:
315:
311:
308:
304:
303:FIM-43 Redeye
301:
292:
289:
281:
277:
271:
265:
261:
256:
252:
244:
240:
236:
232:
228:
224:
220:
215:
211:
207:
203:
199:
195:
191:
187:
183:
178:
175:
171:
167:
163:
156:
152:
148:
145:
142:
138:
134:
130:
127:
124:
120:
115:
112:
108:
104:
100:
96:
92:
88:
85:
81:
78:
77:
72:
68:
64:
60:
55:
52:United States
51:
47:
43:
39:
32:
27:
20:
3439:Rainbow code
3390:
3261:Undesignated
2435:
2134:the original
2125:
2102:. Retrieved
2098:the original
2093:
2083:
2072:
2061:. Retrieved
2057:the original
2047:
2028:
1976:
1970:
1958:
1946:
1934:
1925:
1916:
1908:
1907:, May 1963,
1904:
1896:
1887:
1878:
1869:
1860:
1851:
1842:
1833:
1813:
1807:
1799:
1787:
1775:
1756:
1745:. Retrieved
1741:the original
1731:
1720:. Retrieved
1713:the original
1704:
1683:
1671:
1659:
1647:
1635:
1630:, p. 9.
1623:
1618:, p. 8.
1603:, p. 6.
1588:, p. 4.
1581:
1576:, p. 2.
1561:, p. 1.
1554:
1540:
1532:
1528:
1520:
1493:|title=
1442:
1390:Soviet Union
1383:
1332:West Germany
1241:Saudi Arabia
1090:
976:Seeker type
799:
791:
785:
777:
771:
765:
730:
673:, including
663:
655:
635:
630:
628:
624:
608:Sukhoi Su-25
597:
572:rocket motor
568:
564:
553:
549:
541:
519:, to assess
505:
497:
490:
432:Marine Corps
429:
418:
397:
386:At the 1950
385:
361:
356:machine guns
341:
307:man-portable
302:
297:
173:
140:Manufacturer
74:
70:Used by
3358:Senior Prom
2396:LGM-35 (II)
2053:"Startsida"
1176:El Salvador
652:Description
525:flight test
353:M2 Browning
333:Development
253:Impact Fuze
161: built
87:Vietnam War
3418:Categories
3075:AGM-158A/B
2391:AQM-35 (I)
2063:2014-08-31
1816:(3384):91.
1747:2009-08-31
1722:2015-09-16
1676:Cagle 1974
1664:Cagle 1974
1640:Cagle 1974
1628:Cagle 1974
1616:Cagle 1974
1601:Cagle 1974
1586:Cagle 1974
1574:Cagle 1974
1559:Cagle 1974
1515:, p. 3702.
1454:References
1361:Guerrillas
964:all-aspect
955:Tail-chase
622:missiles.
600:mujahideen
517:California
247:Detonation
3391:See also:
3303:Have Dash
2667:AGM-84H/K
2366:MGM-31A/B
1459:Citations
1424:– (
1412:– (
1400:– (
1388:– (
1109:Australia
1091:Sources:
1074:Operators
612:Mil Mi-24
419:In 1955,
322:July 1971
249:mechanism
153:1962–1971
135:July 1959
76:Operators
65:1967–1995
3166:AIM-174B
3080:AGM-158C
2817:BGM-109G
2714:"AIM-92"
2104:30 April
1911:(5):102.
1764:Archived
1484:cite web
1409:Misagh-2
1402:Pakistan
1371:See also
1293:Thailand
1228:Pakistan
979:Uncooled
792:XFEM-43C
778:XFEM-43B
736:and the
681:Variants
584:Mil Mi-6
344:infantry
284:Guidance
201:Diameter
174:Variants
169:Variants
150:Produced
132:Designed
122:Designer
111:Mali War
3368:Wagtail
3348:OpFires
3268:Aequare
3252:MIM-401
3247:AIM-260
3231:AGM-187
3226:MQM-186
3221:MQM-185
3216:RGM-184
3211:AGM-183
3206:LGM-182
3201:AGM-181
3196:AGM-180
3191:AGM-179
3186:MQM-178
3181:BQM-177
3176:AGM-176
3171:MQM-175
3162:RIM-174
3157:GQM-173
3152:FGM-172
3147:MQM-171
3142:MQM-170
3137:AGM-169
3132:MGM-168
3127:BQM-167
3122:MGM-166
3117:RGM-165
3112:MGM-164
3107:GQM-163
3102:RIM-162
3097:RIM-161
3092:ADM-160
3087:AGM-159
3070:MGM-157
3065:RIM-156
3060:BQM-155
3055:AGM-154
3050:AGM-153
3045:AIM-152
3040:FQM-151
3033:151–200
3024:PQM-150
3019:PQM-149
3014:FGM-148
3009:BQM-147
3004:MIM-146
2999:BQM-145
2994:ADM-144
2989:MQM-143
2984:AGM-142
2979:ADM-141
2974:MGM-140
2969:RUM-139
2964:CEM-138
2959:AGM-137
2954:AGM-136
2949:ASM-135
2944:MGM-134
2939:UGM-133
2934:AIM-132
2929:AGM-131
2924:AGM-130
2919:AGM-129
2914:AQM-128
2909:AQM-127
2904:BQM-126
2894:AGM-124
2889:AGM-123
2884:AGM-122
2874:AIM-120
2869:AGM-119
2864:LGM-118
2859:FQM-117
2854:RIM-116
2849:MIM-115
2844:AGM-114
2839:RIM-113
2834:AGM-112
2829:BQM-111
2824:BGM-110
2807:BQM-108
2802:MQM-107
2797:BQM-106
2792:MQM-105
2787:MIM-104
2782:AQM-103
2777:PQM-102
2772:RIM-101
2765:101–150
2756:LIM-100
2662:AGM-84E
2466:XLIM-49
2370:MGM-31C
2334:LGM-25C
2329:HGM-25A
1535:(7):18.
1254:Somalia
1163:Denmark
1150:Croatia
880:Length
814:System
800:FIM-43D
751:foxhole
642:Contras
594:History
531:began.
502:Testing
421:Convair
230:Warhead
126:Convair
3363:Sprint
2751:LIM-99
2746:YQM-98
2741:AIM-97
2736:UGM-96
2731:AIM-95
2726:YQM-94
2721:XQM-93
2709:FIM-92
2704:AQM-91
2699:BQM-90
2694:UGM-89
2689:AGM-88
2684:AGM-87
2679:AGM-86
2674:RIM-85
2652:AGM-83
2647:AIM-82
2642:AQM-81
2637:AGM-80
2632:AGM-79
2627:AGM-78
2622:FGM-77
2617:AGM-76
2612:BGM-75
2607:BQM-74
2602:UGM-73
2597:MIM-72
2592:BGM-71
2587:LEM-70
2582:AGM-69
2577:AIM-68
2572:RIM-67
2567:RIM-66
2562:AGM-65
2557:AGM-64
2552:AGM-63
2547:AGM-62
2542:MQM-61
2537:AQM-60
2532:RGM-59
2527:MQM-58
2522:MQM-57
2517:PQM-56
2512:RIM-55
2507:AIM-54
2502:AGM-53
2497:MGM-52
2492:MGM-51
2485:51–100
2476:RIM-50
2471:LIM-49
2461:AGM-48
2456:AIM-47
2451:MIM-46
2446:AGM-45
2441:UUM-44
2436:FIM-43
2431:MQM-42
2426:AQM-41
2421:MQM-40
2416:MQM-39
2411:AQM-38
2406:AQM-37
2401:MQM-36
2386:AQM-34
2381:MQM-33
2376:MGM-32
2361:LGM-30
2356:MGM-29
2351:AGM-28
2346:UGM-27
2341:AIM-26
2324:RIM-24
2319:MIM-23
2314:AGM-22
2309:MGM-21
2304:ADM-20
2299:PGM-19
2294:MGM-18
2289:PGM-17
2284:CGM-16
2279:RGM-15
2274:MIM-14
2264:AGM-12
2259:PGM-11
2254:CIM-10
2035:
1983:
1359:Contra
1338:Groups
1329:
1316:
1306:Turkey
1303:
1290:
1280:Sweden
1277:
1264:
1251:
1238:
1225:
1215:Jordan
1212:
1202:Israel
1199:
1189:Greece
1186:
1173:
1160:
1147:
1134:
1120:
1106:
1095:States
755:CONARC
743:cooled
675:flares
631:Hamlet
445:Lancer
286:system
263:Engine
193:Length
164:85,000
3378:GLSDB
3338:NCADE
3328:MA-31
3278:Brazo
3273:ASALM
2249:AIM-9
2244:RIM-8
2237:RIM-7
2232:AIM-7
2227:RGM-6
2222:MGM-5
2217:AIM-4
2212:MIM-3
2207:RIM-2
2202:MGM-1
2137:(PDF)
2130:(PDF)
1716:(PDF)
1709:(PDF)
1434:Notes
1384:Grail
1382:SA-7
1267:Sudan
957:only
945:HTA-3
845:1968
842:1974
839:1968
372:radar
305:is a
3353:PrSM
3343:NLOS
3333:MSDM
3323:LRHW
3318:LREW
3298:HACM
3293:HALO
3240:201–
2195:1–50
2106:2010
2033:ISBN
1981:ISBN
1497:help
1426:Iran
1421:Qaem
1414:Iran
1397:Anza
1365:FMLN
1137:Chad
667:fuze
616:Mi-8
614:and
511:and
461:SLAM
368:0.60
298:The
209:Crew
185:Mass
172:See
83:Wars
73:See
41:Type
3313:KEI
3308:JSM
3288:GBI
1814:105
1349:FAN
937:HMX
931:HMX
638:FDN
468:of
159:No.
3420::
2092:.
1995:^
1909:43
1903:,
1821:^
1806:,
1695:^
1608:^
1593:^
1566:^
1533:13
1527:,
1505:^
1488::
1486:}}
1482:{{
1467:^
648:.
515:,
483:,
472:,
452:,
411:.
3164:/
2372:)
2368:(
2179:e
2172:t
2165:v
2108:.
2066:.
2041:.
1989:.
1750:.
1725:.
1499:)
1495:(
1478:.
1428:)
1416:)
1404:)
1392:)
962:(
576:g
476:,
456:,
212:1
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
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