HJT-36 Yashas | |
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![]() Side shot of the HJT-36 at Yelahanka Air Force Base | |
General information | |
Type | Intermediate trainer |
National origin | India |
Manufacturer | Hindustan Aeronautics Limited |
Designer | Aircraft Research and Design Centre |
Status | Limited series production |
Primary users | Indian Air Force |
Number built | 16 [1] |
History | |
Introduction date | 2026 (Planned) |
First flight | 7 March 2003 |
Developed from | HJT-16 Kiran |
Developed into | HAL HLFT-42 |
The HAL HJT-36 Yashas is a subsonic intermediate jet trainer aircraft designed and developed by Aircraft Research and Design Centre (ARDC) [2] 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. [3]
The jet, originally named Sitara, was designed as 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]
During the opening ceremony of Aero India 2025, the HJT-36 was renamed as Yashas after undergoing significant design modifications. It is now capable of Stage II pilot training, counter insurgency and counter surface force operations, armament training, aerobatics and other roles. [7]
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 at the cost of ₹ 180 crore (equivalent to ₹773 croreorUS$89 million in 2023). The completion of the contract was scheduled in July 2004. [8]
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. [32] The pilots have both conventional and manual flight controls. [33]
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. [32]
The cockpit features a Stepped-up Rear cockpit with a Drooped Nose enhancing the pilots' situational awareness. The aircraft also features multi-function displays and head-up display. . [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. [31]
The aircraft features a FADEC-controlled NPO Saturn AL-55I with a thrust of 17.3 kN, providing a high thrust-to-weight ratio with optimised thrust management. [7]
The prototype aircraft was initially powered by a SNECMA Turbomeca Larzac 04-H-20 non-afterburning turbofan developing 14.12 kN of thrust. [9] However, as stipulated by the 2005 Air Staff Qualitative Requirements (ASQRs) from the Air Force there was a requirement of higher thrust engines. [34]
In April 2005, the Larzac engine was to be replaced by NPO Saturn AL-55I (16.9 kN) to meet training requirements. The AL-55I engine would be a Joint Venture of HAL and NPO Saturn and the deal for the development of the same was signed with Rosoboronexport in August. A funding of ₹ 159 crore (equivalent to ₹540 croreorUS$62 million in 2023) by the Indian Ministry of Defence was released for the higher thrust engine development. [8] [10]
As per a CAG report on IJT, in February 2014, the engine developed (AL-55I) had a Total Technical Life (TTL) of only 300 hours against the required 3600 hours provided in the ASQR. However, by 2013, it was told that the contract for engine development was fulfilled and the JV intended to increase the TTL to 600 hours though IAF insisted a TTL of 1,200 hours. The increase of TTL was important as ASQR projected a "utilisation rate" of 30 hrs/month per aircraft which meant the engines needed to be replaced every 10 months. [10] [9]
On 14 July 2021, it was reported that the United Engine Corporation had deliver two units of AL-55I engines to HAL for the HJT-36 programme. The life cycle of the improved engines were increased to 1,200 hours . Earlier, 16 engines had been supplied to HAL for the prototypes and limited series production (LSP) aircraft. The engines were reportedly ready for licenced production in India. [30] [35] [36] The new engines also had an improved thrust of 17.27 kN and also featured a reduction of over 50 kg weight. [9]
Data from Jane's All the World's Aircraft [37] [38]
General characteristics
Performance
Armament
Related development
Aircraft of comparable role, configuration, and era
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