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HAL HJT-36 Sitara

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well as weapon and drop tank trials. The activities left for obtaining Final Operational Clearance (FOC) are the refinement of stall characteristics, and spin testing which will be commenced as soon as stall characteristics were refined. All efforts were being made to achieve FOC by December 2014. Production of aircraft was to commence immediately thereafter. However the stall cannot be tested until HAL redesigns the entire aircraft to correct its "inherent asymmetry".
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On 19 February 2014, the Indian MOD submitted a statement that the development of IJT was in the advanced stages of certification, with more than 800 test flights completed so far. The activities were progressing well with completion of sea level trials, night flying trials, high altitude trials as
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awarded HAL a contract for the development, testing, and certification of two prototype IJT aircraft. HJT-36 uses light alloys and composites, with a conventional low wing design with 18° leading-edge sweepback and a 9.8m wingspan. It features a hydraulically retractable tricycle-type landing gear.
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is a conventional jet trainer with low swept wings, tandem cockpit and small air intakes for the engine on either side of its fuselage. It entered limited series production by 2010 but according to the Indian Air Force officials it remained "unfit" for service due to technological issues related to
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was consulted on certain design changes, specifically the tail. Afterwards the design was put to mathematical and wind tunnel tests. The modified aircraft was expected to complete the spin tests by September 2015, and the production of 85 aircraft for the Indian Air Force to
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In the cockpit, the HJT-36 has a conventional tandem two-seat configuration with the trainee pilot forward and the instructor in the raised seat to the rear. The single-piece canopy gives both pilots good, all-round vision. The prototype aircraft used
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The aircraft has five external hardpoints for weapons training. There is one center-line hardpoint under the fuselage and two-weapon pylons under each wing for carrying rockets, gun pods, and bombs. The maximum external payload is 1,000 kg.
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Further delays were caused by delays in delivery of the NPO Saturn engine by 2 years, as well as due to two accidents in February 2007 and in February 2009 involving each of the prototypes, which grounded the aircraft for repairs and
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reported that due to the HJT-36's "unsolvable" issues associated with critical stall and spin characteristics the aircraft is not ready to serve as an intermediate jet trainer for Indian Air Force pilots.
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The first and second prototypes of the HJT-36, labeled PT-1 and PT-2, flew on 7 March 2003 and in March 2004, respectively. The program was then delayed with the Air Force assessing the
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The single-wheeled main units retract inward and the twin nose wheel unit retracts forward. About a quarter of the aircraft's line replaceable units are common between it and the
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placed an order for 73 aircraft. After over 280 test flights, the aircraft entered limited series production in 2009 for the first 12 aircraft to be delivered to the Air Force.
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on 28 December 2008, 2 years later than committed, and was installed on PT-1. Following ground taxiing trials, flight tests with the new engine started on 9 May 2009.
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The trainer has a full glass cockpit with a layout similar to current generation combat aircraft. It uses an integrated digital avionics system from
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HAL started design work on an intermediate jet trainer in 1997. The concept was developed as a successor to HAL's earlier trainer, the HJT-16
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engine, with 14.1 kN of thrust, as under-powered. In response, in August 2005, HAL reached a deal to replace the SNECMA engine with the
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On 6 January, the IJT has successfully demonstrated the capability to carry out six turn spins to both the left and right hand sides.
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Mk.16 IN16S seats, due to a price escalation of the former. The pilots have both conventional and manual flight controls.
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further down which is expected to make spin recovery easier. The modified aircraft flew for the first time in April 2019.
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AL-55I with 16.9 kN of thrust. The deal also provided for license-production of the engine in India by HAL.
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engine with about 16.9 kN of thrust, as stipulated by the 2005 air staff requirements from the Air Force.
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Jackson, Paul; Peacock, Lindsay; Bushell, Susan; Willis, David; Winchester, Jim, eds. (2016–2017). "India".
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flew for the first time in three years with a modified air frame to correct its spin characteristics.
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1 × under-fuselage and 4 × under-wing pylons with a capacity of 1,000 kilograms (2,200 lb)
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HAL Intermediate Jet Trainer HJT-36 by Wg.Cdr Kukke Suresh VrC(Retd.) @ Bharat-rakshak.com
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was expected by July 2011. The Air Force order was expected to grow to over 200 aircraft.
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spin test (as of March 2017)., an issue which was only solved in tests in January 2022.
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Bharat-Rakshak Monitor: Sitara - Intermediate Jet Trainer - HJT-36 by H. Niranjan Rao
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developing 14.12 kN of thrust. All production models will use the more powerful
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The first flight test for the limited series aircraft occurred in January 2010, and
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designed and developed by Aircraft Research and Design Centre (ARDC) and built by
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non-afterburning turbofan, 14.12 kN (3,175 lbf) thrust (Prototypes)
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In December 2013, HAL declared that Sitara was 'weeks' from certification.
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On 27 July 2012, first Engine Ground Run was performed on third prototype.
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With Birhle as a consultant, the air frame was modified to move the
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ACIG Exclusive: 15 Photos of two HJT-36 prototypes and its cockpit
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IHS Jane's All the World's Aircraft: Development & Production
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After further development and extensive testing, the
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Aircraft of comparable role, configuration, and era
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Side shot of the HJT-36 at Yelahanka Air Force Base
287:The prototype aircraft was initially powered by a 1408:Photos of the two prototypes @ Bharat-rakshak.com 769: 767: 1896: 934:. 9 February 2007 – via www.thehindu.com. 920: 764: 276:. Head-up display and repeater is produced by 1433: 1012:. Chennai, India. 14 May 2009. Archived from 928:"Jet trainer overshoots runway at aero show" 854:"HAL HJT-36 Sitara - program supplier guide" 1200:Simha, Rakesh Krishnan (24 February 2014). 1028: 224: 1440: 1426: 1357:: CS1 maint: location missing publisher ( 848: 846: 583:308.6 kg/m (63.21 lb/sq ft) 339:The first AL-55I engine was received from 1326: 1187:"HJT-36 Target FOC By Dec 2014, Says MoD" 996: 914:"HAL HJT-36 | Aviation Week Network" 565:1,000 km (621 mi, 540 nmi) 553:750 km/h (466 mph, 405 kn) 1034: 875:"HJT-36 Sitara Intermediate Jet Trainer" 869: 867: 306: 228: 843: 830: 14: 1910:2000s Indian military trainer aircraft 1897: 1279: 1165: 1133:: CS1 maint: archived copy as title ( 971: 265:. However, these may be replaced with 1421: 1226: 1199: 1184: 864: 712: 1298: 1246:D.S, Madhumathi (9 September 2015). 804: 495:4.4 m (14 ft 5.25 in) 1449:Hindustan Aeronautics Limited (HAL) 1245: 501:17.5 m (188.4 sq ft) 489:10 m (32 ft 9.75 in) 449:Specifications (HJT-36, prototypes) 90:Aircraft Research and Design Centre 24: 452: 199:. The HJT-36 will replace the HAL 183:") is a subsonic intermediate jet 25: 1936: 1391: 1166:Shukla, Ajai (20 December 2013). 1035:Krishnan, Anantha (28 May 2010). 1299:Peri, Dinakar (7 January 2022). 1185:Aroor, Shiv (19 February 2014). 805:Peri, Dinakar (7 January 2022). 773: 624: 610: 483:11 m (36 ft 1 in) 40: 1365: 1292: 1273: 1239: 1220: 1193: 1178: 1159: 1095: 1077: 1059: 938: 906: 831:Waldron, Greg (18 April 2019). 713:Pubby, Manu (9 February 2020). 463:Jane's All the World's Aircraft 311:Prototype IJT in its hangar at 289:SNECMA Turbomeca Larzac 04-H-20 1280:Shukla, Ajai (19 April 2019). 1174:– via Business Standard. 892: 824: 798: 750: 725: 706: 522:5,400 kg (11,905 lb) 362:initial operational capability 302: 13: 1: 1248:"IAF's IJT set for spin test" 699: 571:9,000 m (29,520 ft) 528:917 kilograms (2,022 lb) 516:4,250 kg (9,370 lb) 313:Hindustan Aeronautics Limited 189:Hindustan Aeronautics Limited 81:Hindustan Aeronautics Limited 1925:Aircraft first flown in 2003 1227:Pubby, Manu (14 July 2018). 7: 1915:Single-engined jet aircraft 603: 235:Yelahanka Air Force Station 233:S3466 HAL HJT-36 Sitara at 10: 1941: 1149:"Press Information Bureau" 1887:(*) are under development 1885: 1855: 1834: 1813: 1782: 1775: 1758: 1736: 1729: 1712: 1691: 1668: 1630: 1586: 1555: 1529: 1464:Manufacturer designations 1463: 1456: 1337:. Couldson. p. 304. 156: 146: 138: 130: 125: 117: 102: 98:Limited series production 94: 86: 74: 64: 56: 51: 39: 31: 1085:"Vayu aerospace article" 318: 263:zero-zero ejection seats 225:Design & development 1172:Business Standard India 468:General characteristics 438: 420: 406: 388: 378: 368: 347: 326:SNECMA Turbomeca Larzac 457: 315: 237: 782:. IHS. Archived from 456: 310: 232: 952:. 28 December 2008. 536:SNECMA Larzac 04-H20 60:Intermediate trainer 1208:. Российская газета 1073:. 10 February 2011. 879:Airforce Technology 639:Related development 520:Max takeoff weight: 274:GE Aviation Systems 261:K-26LT lightweight 246:Government of India 52:General information 1233:The Economic Times 1115:on 16 January 2013 1071:The Times of India 1047:on 23 January 2018 458: 316: 238: 1920:Low-wing aircraft 1892: 1891: 1881: 1880: 1771: 1770: 1730:Jointly developed 1725: 1724: 1286:Business Standard 858:www.airframer.com 297:NPO Saturn AL-55I 291:non-afterburning 253:trainer variant. 166: 165: 131:Introduction date 16:(Redirected from 1932: 1783:Fighter aircraft 1780: 1779: 1737:Fighter aircraft 1734: 1733: 1587:Fighter aircraft 1461: 1460: 1442: 1435: 1428: 1419: 1418: 1385: 1384: 1382: 1380: 1369: 1363: 1362: 1356: 1348: 1330: 1324: 1323: 1321: 1319: 1296: 1290: 1289: 1277: 1271: 1270: 1268: 1266: 1243: 1237: 1236: 1224: 1218: 1217: 1215: 1213: 1197: 1191: 1190: 1182: 1176: 1175: 1163: 1157: 1156: 1145: 1139: 1138: 1132: 1124: 1122: 1120: 1114: 1108:. 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Index

HAL HJT-36

India
Manufacturer
Hindustan Aeronautics Limited
Indian Air Force
Indian Navy
HJT-16 Kiran
HAL HJT 39
Sitārā
Star
trainer aircraft
Hindustan Aeronautics Limited
Indian Air Force
Indian Navy
HJT-16 Kiran

Yelahanka Air Force Station
Government of India
HAL Tejas
Zvezda
zero-zero ejection seats
Martin-Baker
GE Aviation Systems
Elbit Systems
SNECMA Turbomeca Larzac 04-H-20
turbofan
NPO Saturn AL-55I

Hindustan Aeronautics Limited

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