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HAL Ajeet

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358: 384:, housing aviation fuel in the interior space within the wing. This had several effects on the overall design, including the substantial expansion of its internal fuel capacity and the freeing up of several underwing hardpoints that had been previously occupied by external fuel tanks, allowing for their use in the carriage of other equipment and armaments. Furthermore, the carriage of even-greater payloads was also enabled via the installation of an additional pair of underwing hardpoints. 26: 470: 225:. The satisfactory performance of these prototypes contributed to the issuing of a production order for the Ajeet. On 30 September 1976, the first production aircraft performed its maiden flight. Introduced to service during the following year, the Ajeet had a relatively brief and unremarkable service life, equipping only a single IAF squadron and being withdrawn from service during 1991. 349:
and pessimism over the project's value from officials heavily contributed to the trainer initiative being curtailed without any further examples being produced. The two surviving aircraft were dispatched to briefly serve with the IAF's No.2 Squadron, where they were used until the phaseout of the Ajeet was completed during 1991.
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flight. Despite this, as late as 1979, additional development tasks and changing requirements were being added onto the programme; these were attributed by defense analyst Amit Gupta as having caused the Ajeet's associated costs to substantially rise as well as having led to setbacks in the programme's manufacturing effort.
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Having fallen out of political favour, fewer than a hundred Ajeets were ultimately procured and the whole programme was effectively terminated barely a decade after its initiation. The aircraft built had relatively short and uneventful careers, and were retired from IAF service during 1991. The Ajeet
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observed that there was little need for a trainer version of the Ajeet as the original Gnat had already been developed into a training aircraft and therefore could have been acquired already if the IAF had the desire to do so. The twin factors of the anticipated imminent phaseout of the Ajeet fighter
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During the late 1970s and early 1980s, HAL undertook work on a project intending to produce a training-oriented variant of the Ajeet. During 1982, this programme had progressed to the point where the initial flight of a prototype for evaluation purposes occurred. This sole aircraft was soon lost in
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According to aviation author Pushpindar Chopra, the design of the Gnat had both positive and negative attributes; while being inexpensive to construct and to operate, several of the onboard systems had been allegedly prone to low levels of reliability, particularly the control system of the aircraft,
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Accordingly, while the Gnat had been determined to be effective as a combat aircraft, it was also viewed that there was room for improvement on the design of its subsystems. During 1972, the IAF therefore issued a formal requirement, calling for the development and production of an improved model of
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During 1977, the HAL Ajeet was accepted into operational service with the IAF. However, only one squadron of the IAF ultimately operated the type, this being No.2 Squadron. According to political author Chris Smith, the lack of enthusiasm on the part of the IAF for the Ajeet was down to a change in
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while the second prototype following on 5 November that year. The flight testing phase of the programme reportedly validated the success of the re-designed aircraft, leading to a production order being placed for the Ajeet. On 30 September 1976, the first production aircraft performed its maiden
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for "Invincible" or "Unconquered". As the design developed, differences between the Ajeet and the original model of the Gnat that had served as its starting point became considerable. During the development process, deliberate efforts were made to rectify the encountered shortcomings and troubles
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role for the new model as well. According to a report by the Public Accounts Committee of the Indian Parliament, the IAF officials tasked with overseeing the programme lacked realistic concepts of what was involved in the development process nor firm ideas on what the aircraft was required for.
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for other purposes, effectively increasing both the range and payload capability of the aircraft. On 6 March 1975, the first of two Ajeet prototypes, producing via the conversion of the final two licence-produced Gnat fighters, conducted its
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speeds had also grown, as such, the Ajeet contrasted poorly with these new priorities. However, also according to Smith, the Ajeet benefitted both from the positive combat reputation garnered by the Gnat, as well as for its relatively low
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while some aspects had proved to be difficult to maintain. The reliability issues had been a known contributing factor to several accidents which had resulted in the total loss of individual Gnats and the deaths of several pilots.
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In support of the development programme, HAL decided to modify the final pair of Gnats on the production line to serve as prototypes for the Ajeet. On 6 March 1975, the first of these prototypes conducted its
369:, while also being capable of ground-attack missions. Being a derivative of the earlier Gnat, the aircraft appeared to be visually similar to its predecessor; the presence of a pair of extra underwing 377:
and onboard systems than the original design. However, the addition of these extra subsystems and features was not without consequence, as the Ajeet was less agile than the original Gnat.
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In response to the issuing of the original requirement, HAL set about designing their revision of the Gnat. Their work was greatly aided by an earlier decision by India to, upon the
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In the design phase of the Ajeet, HAL redesigned several aspects of the aircraft while seeking to improve both the reliability and effectiveness of several subsystems, such as the
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An Ajeet and four privately owned Gnat T.1s portrayed the fictional carrier-based "Oscar EW-5894 Phallus" tactical fighter bombers flown by US Navy pilots in the 1991 comedy
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arrangement, and refined control systems, to produce superior performance, compared to their original counterparts. The control surfaces were enhanced via the adoption of a
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during the 1960s, acquire many former assets of the company. The residual rights for the type had been transferred to the IAF while other items, such as the
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by HAL, had acquitted itself favourably during its Indian service, including in active combat roles during multiple conflicts with Pakistan, including the
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During its service life with the IAF, the Gnat proved to be relatively successful when deployed for active combat missions. The type was used in both the
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attitudes; the service had allegedly become increasingly opposed to the use of single-engine aircraft while a preference for fighters capable of
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However, information on the Ajeet trainer programme was received with a lack of interest on the part of the Indian government. IAF Air Commodore
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being amongst the only obvious distinguishing features from the older Gnat. In general, the Ajeet was equipped with a variety of more capable
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a crash later that same year. The following year, a second prototype performed its maiden flight and was closely followed by a third.
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Gupta, Amit. "Building an Arsenal: The Evolution of Regional Power Force Structures." Greenwood Publishing Group, 1997.
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During the 1950s, the government of India had come to an agreement with the United Kingdom to procure a large number of
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missions and to perform short range ground attack runs. Due to its effectiveness against Pakistani fighters, such the
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the Gnat. Although the original revision of the requirement had called for the type to be produced to function as an
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and test apparatus, had been moved to HAL. Early on, the fledgling aircraft design received the name "Ajeet",
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Smith, Chris. "India's Ad Hoc Arsenal: Direction Or Drift in Defence Policy?" Oxford University Press, 1994.
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configuration, which was unique to the Ajeet. It was also decided to outfit the aircraft with improved
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4 with a capacity of 900 kg (2,000 lb) total, with provisions to carry combinations of:
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1,034 m (3,400 ft) ISA at 4,136 kg (9,118 lb), 2x rocket pod and 2x drop tanks
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Certain aspects of the aircraft were heavily redesigned from the Gnat, such as the much enhanced
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The HAL Ajeet was a jet-propelled light fighter, primarily intended to function as a low-level
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Singh, Jasjit. "Indian Air Force: The Case for Indigenisation." KW Publishers Pvt Ltd, 2013.
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light fighter aircraft. The Gnat, which had been procured in large numbers for the IAF and
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172 km (107 mi, 93 nmi) lo-lo-lo, with two 250 kg (551 lb) bombs
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against neighbouring Pakistan. Operationally, it was used to conduct both low-level
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One of the more significant changes made for the Ajeet was the addition of a
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expanded the fighter's internal fuel capacity and freed-up several underwing
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The prototype Ajeet, E1083, preserved outside HAL's headquarters in Bangalore
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2x 136.5 L (36.1 US gal; 30.0 imp gal) drop tanks
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Khan, J. A. "Air Power And Challenges To IAF." APH Publishing, 2004.
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15° at 4,136 kg (9,118 lb), 2x rocket pod and 2x drop tanks
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30° at 4,136 kg (9,118 lb), 2x rocket pod and 2x drop tanks
441: : The original Indian Air Force designation for the Ajeet Mk 1. 370: 217: 171: 1230:, June 1977, Vol 12 No 6. Bromley, UK:Fine Scroll. pp. 284–290. 1504: 1483: 1411: 916: 608: 381: 374: 319: 213: 205: 568: 1353: 1273:
Kumar, Satish. "India’s National Security: Annual Review 2009."
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5.3g ISA at 834 km/h (518 mph; 450 kn), sea level
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1,134 km/h (705 mph; 612 kn) at sea level ISA
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1,152 km/h (716 mph, 622 kn) at sea level ISA
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1,102 km/h (685 mph; 595 kn) at sea level ISA
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15° at 834 km/h (518 mph; 450 kn), sea level
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30° at 834 km/h (518 mph; 450 kn), sea level
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Folland Gnat / HAL Ajeet from Greg Goebel's Air Vectors
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12,000 m (39,000 ft) in 6 minutes 2 seconds
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Aircraft of comparable role, configuration, and era
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3,539 kg (7,802 lb) clean take-off weight
361:IAF Ajeet on undergoing cosmetic restoration, 2016 323:discovered within the design of the earlier Gnat. 457: : Two-seat advanced jet training prototype. 1802: 952: 1163: 1123: 1121: 677:M0.953 at 12,000 m (39,000 ft), ISA 662:M0.948 at 12,000 m (39,000 ft), ISA 1339: 1156: 1154: 716:328.8 kg/m (67.3 lb/sq ft) max 507: 1144: 1142: 1045: 1043: 1041: 1039: 1037: 684:M0.96 at 12,000 m (39,000 ft), ISA 1118: 1097: 1088: 1063: 1061: 1059: 1057: 1055: 153: 1346: 1332: 1151: 1111: 1109: 611:engine, 20 kN (4,500 lbf) thrust 1139: 1034: 429:was never deployed in combat operations. 185:The Ajeet is a derivative of the British 1070: 1052: 356: 1831:India–United Kingdom military relations 1249:Jane's All The World's Aircraft 1982–83 1181:"The Incomplete Guide to Airfoil Usage" 1106: 1017:List of aircraft of the Royal Air Force 606:TJE HAL/Bristol Siddeley Orpheus 701-01 516:Jane's All The World's Aircraft 1982–83 1803: 410: 335: 1327: 1172: 813:658 m (2,200 ft) ISA at NLW 779:951 m (3,120 ft) ISA at NLW 495: 170:developed and manufactured by Indian 1178: 555:12.69 m (136.6 sq ft) 277:, the type was given the moniker of 1355:Hindustan Aeronautics Limited (HAL) 288: 13: 893:2x 250 kg (551 lb) bombs 543:6.73 m (22 ft 1 in) 537:9.04 m (29 ft 8 in) 14: 1847: 1312: 1251:. London:Jane's Yearbooks, 1982. 759:1,047 m (3,435 ft) ISA 738:1,180 m (3,870 ft) ISA 723:1,376 m (4,500 ft) ISA 549:2.46 m (8 ft 1 in) 242:fighters, a light combat-capable 934:TA/RA-22 VHF tx/Rx {V/UHF later) 488:No. 2 Squadron, Indian Air Force 468: 91:89 (including 10 upgraded Gnats) 24: 1217: 1198: 871:2 × 30 mm (1.181 in) 806:695 m (2,280 ft) ISA 791:725 m (2,379 ft) ISA 772:997 m (3,300 ft) ISA 502:List of surviving Folland Gnats 1130: 1079: 704:13,720 m (45,000 ft) 591:4,173 kg (9,200 lb) 228: 178:(HAL). It was operated by the 1: 1816:1970s Indian fighter aircraft 1224:Chopra, Pushpindar. "Ajeet". 1022: 789:Landing run with brake chute: 598:2,767 kg (6,100 lb) 579:2,307 kg (5,086 lb) 256:Hindustan Aeronautics Limited 254:in India by aviation company 233: 182:(IAF) between 1977 and 1991. 176:Hindustan Aeronautics Limited 63:Hindustan Aeronautics Limited 1836:Aircraft first flown in 1976 1027: 953:Notable appearances in media 461: 407:for improved survivability. 7: 1821:Single-engined jet aircraft 966: 937:Bendix BEL AX-3 standby VHF 757:Landing run no brake chute: 432: 212:systems. The adoption of a 10: 1852: 1210:Retrieved 28 January 2024. 922:Ferranti navigation system 919:F195R/3 ISIS weapons sight 508:Specifications (HAL Ajeet) 267:Indo-Pakistani War of 1971 263:Indo-Pakistani War of 1965 199:Indo-Pakistani War of 1971 195:Indo-Pakistani War of 1965 1793:(*) are under development 1791: 1761: 1740: 1719: 1688: 1681: 1664: 1642: 1635: 1618: 1597: 1574: 1536: 1492: 1461: 1435: 1370:Manufacturer designations 1369: 1362: 1127:Chopra 1977, pp. 287–288. 1103:Chopra 1977, pp. 286–287. 1094:Chopra 1977, pp. 284–286. 352: 275:North American F-86 Sabre 145: 124: 116: 108: 100: 95: 87: 76: 68: 56: 48: 40: 35: 23: 18: 500:Survivors are listed at 1185:m-selig.ae.illinois.edu 1169:Taylor 1982, pp. 93–94. 522:General characteristics 596:Normal landing weight: 391:systems, the improved 362: 191:produced under license 397:all-moving tail plane 360: 252:licensing arrangement 1205:"Hot Shots! (1991)." 1160:Chopra 1977, p. 287. 1049:Chopra 1977, p. 288. 660:Maximum Mach number: 367:interceptor aircraft 1148:Kumar 2012, p. 373. 1076:Smith 1994, p. 159. 1067:Smith 1994, p. 160. 1000:Northrop T-38 Talon 972:Related development 589:Max takeoff weight: 423:radar cross-section 411:Operational history 336:Further development 36:General information 1826:High-wing aircraft 1115:Gupta 1997, p. 50. 1085:Khan 2004, p. 137. 1005:T-33 Shooting Star 496:Surviving aircraft 455:Ajeet Mk 2 Trainer 363: 265:and the follow-up 246:aircraft, for the 1798: 1797: 1787: 1786: 1677: 1676: 1636:Jointly developed 1631: 1630: 1227:Air International 1179:Lednicer, David. 940:Bendix DFA-73 ADF 708:Time to altitude: 134: 133: 101:Introduction date 1843: 1689:Fighter aircraft 1686: 1685: 1643:Fighter aircraft 1640: 1639: 1493:Fighter aircraft 1367: 1366: 1348: 1341: 1334: 1325: 1324: 1245:Taylor, John W R 1211: 1202: 1196: 1195: 1193: 1191: 1176: 1170: 1167: 1161: 1158: 1149: 1146: 1137: 1134: 1128: 1125: 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Retrieved 1184: 1174: 1165: 1136:Singh 2013, 1132: 1099: 1090: 1081: 1072: 1010: 1009: 995:Northrop F-5 988: 987: 978:Folland Gnat 971: 970: 958: 956: 906: 904: 896: 890: 884: 878: 868: 860: 858: 842:5.28g - ISA 824: 788: 756: 720: 713: 707: 701: 695: 659: 623: 616: 614: 601: 595: 588: 582: 576: 567: 560:Aspect ratio 558: 552: 546: 540: 534: 528: 521: 519: 515: 512: 511: 499: 454: 444: 438: 427: 414: 401:Martin-Baker 393:landing gear 386: 379: 364: 346:Jasjit Singh 343: 339: 325: 305: 292: 283: 279:Sabre Slayer 278: 260: 240:Folland Gnat 237: 203: 187:Folland Gnat 184: 160: 157:Undefeatable 156: 137: 135: 129:Folland Gnat 112:6 March 1975 109:First flight 88:Number built 77:Primary user 58:Manufacturer 1748:Dornier 228 1720:Helicopters 1537:Helicopters 887:rocket pods 879:Hardpoints: 875:with 90 rpg 617:Performance 602:Powerplant: 308:liquidation 296:interceptor 229:Development 165:jet-powered 1805:Categories 1363:Indigenous 1247:(editor). 1023:References 960:Hot Shots! 810:15° at NLW 795:30° at NLW 776:15° at NLW 763:30° at NLW 553:Wing area: 445:Ajeet Mk 1 418:supersonic 371:hardpoints 234:Background 218:hardpoints 1527:Tejas Mk2 1275:Routledge 1028:Citations 827:5g - ISA 541:Wingspan: 513:Data from 462:Operators 439:Gnat Mk 2 389:hydraulic 210:hydraulic 172:aerospace 138:HAL Ajeet 1774:Prentice 1762:Trainers 1650:Su-30MKI 1549:Prachand 1462:Trainers 1357:aircraft 1277:, 2012. 1190:16 April 967:See also 917:Ferranti 907:Avionics 885:Rockets: 861:Armament 609:turbojet 433:Variants 382:wet wing 375:avionics 320:Sanskrit 214:wet wing 206:avionics 197:and the 163:) was a 152:: Ajīt, 142:Sanskrit 1727:Cheetah 1598:Gliders 1453:Pushpak 1448:Krishak 1387:HAOP-27 573:RAE 102 569:Airfoil 547:Height: 535:Length: 425:(RCS). 117:Retired 96:History 72:Retired 44:Fighter 1753:HS 748 1732:Chetak 1706:MiG-27 1701:MiG-21 1696:Jaguar 1605:Ardhra 1479:Sitara 1469:Deepak 1443:Basant 1427:HJT 39 1422:HTT-40 1417:HUL-26 1407:HJT-36 1402:HJT-16 1397:HPT-32 1303:  1292:  1281:  1266:  1255:  1237:  1208:IMPDb. 932:Bendix 926:Vinten 897:Other: 891:Bombs: 473:  353:Design 69:Status 1769:PC-5A 1588:Saras 1566:Rudra 1544:Dhruv 1522:Tejas 1516:TEDBF 1511:Marut 1500:Ajeet 1474:Kiran 1392:HF-24 1382:HA-31 946:Mk.10 869:Guns: 529:Crew: 476:India 83:(IAF) 52:India 19:Ajeet 1779:Hawk 1711:Gnat 1665:UAVs 1619:UAVs 1505:AMCA 1484:HT-2 1412:HT-2 1301:ISBN 1290:ISBN 1279:ISBN 1264:ISBN 1253:ISBN 1235:ISBN 1192:2019 604:1 × 564:3.56 403:GF4 316:jigs 208:and 154:lit. 150:IAST 146:अजीत 136:The 120:1991 104:1977 41:Type 1610:G-1 1582:RTA 1560:MLH 1554:LUH 1377:G-1 944:IFF 681:15° 666:30° 645:15° 630:30° 310:of 159:or 1807:: 1183:. 1153:^ 1141:^ 1120:^ 1108:^ 1054:^ 1036:^ 963:. 504:. 148:; 144:: 1672:* 1657:* 1626:* 1590:* 1584:* 1562:* 1556:* 1529:* 1518:* 1507:* 1347:e 1340:t 1333:v 1307:. 1296:. 1285:. 1270:. 1259:. 1241:. 1194:. 844:+ 829:+ 808:+ 793:+ 774:+ 761:+ 740:+ 725:+ 679:+ 664:+ 643:+ 628:+ 571:: 562:: 531:1 451:. 140:(

Index


Manufacturer
Hindustan Aeronautics Limited
Indian Air Force
Folland Gnat
Sanskrit
IAST
jet-powered
fighter aircraft
aerospace
Hindustan Aeronautics Limited
Indian Air Force
Folland Gnat
produced under license
Indo-Pakistani War of 1965
Indo-Pakistani War of 1971
avionics
hydraulic
wet wing
hardpoints
maiden flight
Folland Gnat
jet-propelled
Indian Air Force
licensing arrangement
Hindustan Aeronautics Limited
Indo-Pakistani War of 1965
Indo-Pakistani War of 1971
air superiority
North American F-86 Sabre

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