HAL HJT-36 Sitara

From Bharatpedia, an open encyclopedia
(Redirected from HAL HJT-36)
Information red.svg
Scan the QR code to donate via UPI
Dear reader, We need your support to keep the flame of knowledge burning bright! Our hosting server bill is due on June 1st, and without your help, Bharatpedia faces the risk of shutdown. We've come a long way together in exploring and celebrating our rich heritage. Now, let's unite to ensure Bharatpedia continues to be a beacon of knowledge for generations to come. Every contribution, big or small, makes a difference. Together, let's preserve and share the essence of Bharat.

Thank you for being part of the Bharatpedia family!
Please scan the QR code on the right click here to donate.

0%

   

transparency: ₹0 raised out of ₹100,000 (0 supporter)



HJT-36 Sitara
Hindustan HJT-36 Sitara Krivchikov 2007.jpg
Role Intermediate Trainer
Manufacturer Hindustan Aeronautics Limited
Design group Aircraft Research and Design Centre
First flight 7 March 2003
Introduction 2023 (Planned)[1]
Status Limited series production
Primary users Indian Air Force
Indian Navy
Number built 16[2]

The HAL HJT-36 Sitara (Sitārā: "star") is a subsonic intermediate jet trainer aircraft designed and developed by Aircraft Research and Design Centre (ARDC)[3] and built by Hindustan Aeronautics Limited (HAL) for the Indian Air Force and the Indian Navy. The HJT-36 will replace the HAL HJT-16 Kiran as the Stage-2 trainer for the two forces.

The Sitara 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 spin test (as of March 2017).[4], an issue which was only solved in tests in January 2022.[5] In April 2019, Sitara flew for the first time in three years with a modified air frame to correct its spin characteristics.[6]

Design & development[edit]

S3466 HAL HJT-36 Sitara at Yelahanka Air Force Station

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 Kiran, introduced in 1968. In 1999, following reviews by the Indian Air Force, the Government of India 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. 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 HAL Tejas trainer variant.

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 Zvezda K-26LT lightweight zero-zero ejection seats. However, these may be replaced with Martin-Baker Mk.16 IN16S seats, due to a price escalation of the former.[7] The pilots have both conventional and manual flight controls.[8]

The trainer has a full glass cockpit with a layout similar to current generation combat aircraft. It uses an integrated digital avionics system from GE Aviation Systems. Head-up display and repeater is produced by Elbit Systems.[7]

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.

The prototype aircraft was initially powered by a SNECMA Turbomeca Larzac 04-H-20 non-afterburning turbofan developing 14.12 kN of thrust. All production models will use the more powerful NPO Saturn AL-55I engine with about 16.9 kN of thrust, as stipulated by the 2005 air staff requirements from the Air Force.

Development[edit]

Prototype IJT in its hangar at Hindustan Aeronautics Limited

2000s[edit]

  • 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 SNECMA Turbomeca Larzac 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 NPO Saturn AL-55I with 16.9 kN of thrust. The deal also provided for license-production of the engine in India by HAL.[8][unreliable source?]
  • 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 investigations.[9][10]
  • The first AL-55I engine was received from Russia on 28 December 2008, 2 years later than committed, and was installed on PT-1.[11] Following ground taxiing trials, flight tests with the new engine started on 9 May 2009.[12][13]

2010[edit]

  • After further development and extensive testing, the Indian Air Force 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.
  • The first flight test for the limited series aircraft occurred in January 2010,[14] and initial operational capability was expected by July 2011.[15][16] The Air Force order was expected to grow to over 200 aircraft.

2012[edit]

  • On 27 July 2012, first Engine Ground Run was performed on third prototype.[17][18]

2013[edit]

  • In December 2013, HAL declared that Sitara was 'weeks' from certification.[19]

2014[edit]

  • 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 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.[20] However the stall cannot be tested until HAL redesigns the entire aircraft to correct its "inherent asymmetry".[21]
  • BAE Systems was consulted on certain design changes, specifically the tail.[22] 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 begin.[23]

2017[edit]

  • In March 2017, Jane's 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.[4]

2019[edit]

  • With Birhle as a consultant, the air frame was modified to move the tailfin and tailplane further down which is expected to make spin recovery easier. The modified aircraft flew for the first time in April 2019.[24]

2022[edit]

  • On 6th January, the IJT has successfully demonstrated the capability to carry out six turn spins to both the left and right hand sides.[25]

Specifications (HJT-36, prototypes)[edit]

Profil HAL HJT-36.png

Data from Jane's All the World's Aircraft[26][27]

General characteristics

  • Crew: 2
  • Length: 11 m (36 ft 1 in)
  • Wingspan: 10 m (32 ft 9.75 in)
  • Height: 4.4 m (14 ft 5.25 in)
  • Wing area: 17.5 m2 (188.4 sq ft)
  • Aspect ratio: 5.5
  • Gross weight: 4,250 kg (9,370 lb)
  • Max takeoff weight: 5,400 kg (11,905 lb)
  • Fuel capacity: 917 kilograms (2,022 lb)
  • Powerplant: 1 × SNECMA Larzac 04-H20 non-afterburning turbofan, 14.12 kN (3,175 lbf) thrust (Prototypes)
  • Powerplant: 1 × Saturn/UMPO AL-55I non-afterburning turbofan, 17 kN (3,821 lbf) thrust (Production aircraft)

Performance

  • Maximum speed: 750 km/h (466 mph, 405 kn)
  • Maximum speed: Mach 0.75
  • Range: 1,000 km (621 mi, 540 nmi)
  • Service ceiling: 9,000 m (29,520 ft)
  • g limits: +7.0/–2.5
  • Wing loading: 308.6 kg/m2 (63.21 lb/sq ft)

Armament

  • Hardpoints: 1 × under-fuselage and 4 × under-wing pylons with a capacity of 1,000 kilograms (2,200 lb)

See also[edit]

Related development

Aircraft of comparable role, configuration, and era

References[edit]

  1. ↑ "India's HJT-36 Sitara intermediate jet trainer begins spin flight testing". 24 November 2022.
  2. ↑ Pubby, Manu (9 February 2020). "Spin test in July may revive intermediate jet trainer plan". Economic Times.
  3. ↑ "With expected 83 Tejas MK1A orders, ARDC shapes India's upgraded fighter". OnManorama. Retrieved 7 August 2020.
  4. ↑ 4.0 4.1 Bedi, Rahul. "India's HJT-36 Sitara remains 'unfit' for use as intermediate jet trainer". Jane's 360. IHS. Retrieved 27 July 2022.
  5. ↑ Peri, Dinakar (7 January 2022). "Intermediate Jet Trainer has cleared a major milestone, says HAL chief". The Hindu. Retrieved 20 October 2022.
  6. ↑ Waldron, Greg (18 April 2022). "PICTURES: HAL HJT-36 IJT flies after three year hiatus". Flightglobal.com.
  7. ↑ 7.0 7.1 "HAL HJT-36 Sitara - program supplier guide". www.airframer.com.
  8. ↑ 8.0 8.1 "HJT-36 Sitara Intermediate Jet Trainer". Airforce Technology. Retrieved 7 January 2022.
  9. ↑ "Jet trainer overshoots runway at aero show". The Hindu. 9 February 2007 – via www.thehindu.com.
  10. ↑ "Login to read". www.blogger.com.[permanent dead link]
  11. ↑ "Russian engines coming today for intermediate jet trainer". The Hindu. 28 December 2008. ISSN 0971-751X. Retrieved 7 January 2022.
  12. ↑ "IJT". Deagel. Retrieved 7 January 2022.{{cite web}}: CS1 maint: url-status (link)
  13. ↑ "HAL's intermediate jet trainer HJT-36 makes maiden flight with Russian engine". The Hindu. Chennai, India. 14 May 2009. Archived from the original on 16 May 2009. Retrieved 12 July 2010.
  14. ↑ Krishnan, Anantha (28 May 2022). "India Thought Leaders: HAL Chairman Sets Firm Agenda For Aggressive Export Sales". aviationweek.com.
  15. ↑ "Indigenous jet trainer to get initial clearance by July". The Times of India. 10 February 2022.
  16. ↑ "Vayu aerospace article".
  17. ↑ "Archived copy" (PDF). Archived from the original (PDF) on 16 January 2013. Retrieved 26 September 2012.{{cite web}}: CS1 maint: archived copy as title (link)
  18. ↑ "Press Information Bureau". pib.nic.in.
  19. ↑ Shukla, Ajai (20 December 2013). "In Tejas' shadow, Sitara trainer also poised to enter service". Business Standard India – via Business Standard.
  20. ↑ Aroor, Shiv (19 February 2022). "HJT-36 Target FOC By Dec 2014, Says MoD".
  21. ↑ Simha, Rakesh Krishnan (24 February 2014). "Flameout: Why the IAF won't accept HAL's jet trainer". indrus.in. Российская газета. Retrieved 23 February 2022.
  22. ↑ Pubby, Manu (14 July 2018). "Spin trials to revive intermediate jet trainer programme soon". The Economic Times.
  23. ↑ D.S, Madhumathi (9 September 2015). "IAF's IJT set for spin test". The Hindu. ISSN 0971-751X. Retrieved 7 January 2022.
  24. ↑ Shukla, Ajai (19 April 2022). "HAL's Intermediate Jet Trainer flies again after extensive re-design". Business Standard.
  25. ↑ Peri, Dinakar (7 January 2022). "Intermediate Jet Trainer has cleared a major milestone, says HAL chief". The Hindu. ISSN 0971-751X. Retrieved 7 January 2022.
  26. ↑ Jackson, Paul; Peacock, Lindsay; Bushell, Susan; Willis, David; Winchester, Jim, eds. (2016–2017). "India". IHS Jane's All the World's Aircraft: Development & Production. Couldson. p. 304. ISBN 978-0710631770.{{cite book}}: CS1 maint: location missing publisher (link)
  27. ↑ "HAL IJT". HAL. Retrieved 2 May 2022.

External links[edit]

Retrieved from "https://en.bharatpedia.org/index.php?title=HAL_HJT-36_Sitara&oldid=408403"