Hindustan Aeronautics Limited

HAL HJT-36 Sitara

The HAL HJT‑36 Sitara is a two‑seat, tandem‑configuration, basic jet trainer developed by Hindustan Aeronautics Limited (HAL) for the Indian Air Force and Indian Navy. Development began in the early 1990s, with the prototype rolling out in 1997 and first flight on 20 January 2000. After an extensive flight‑test programme and several revisions to address handling and engine performance, the aircraft entered limited service in 2009, becoming the first indigenously designed and manufactured jet trainer to attain operational status in India.

Key features include a low‑drag, all‑metal airframe, a retractable tricycle landing gear, and a modern glass cockpit equipped with multifunction displays, flight‑data recording and a Hands‑On‑Throttle‑And‑Stick (HOTAS) interface. Power is supplied by a NPO‑ATK‑67 (formerly Turbomeca) turbofan engine delivering about 16 kN of thrust, providing a maximum speed of Mach 0.78 and a service ceiling of 12 000 m. The Sitara is equipped with provisions for basic armament, allowing weapons‑delivery training.

Its significance lies in reducing India’s reliance on foreign trainers, fostering domestic aerospace expertise, and serving as a platform for pilot conversion to frontline combat aircraft. The HJT‑36 also underpins HAL’s broader ambition to develop advanced jet trainers and light combat aircraft for export and future Indian defence programmes.

Classification

Production & History

First Flight
2003

Design & Classification

Manufacturer
Hindustan Aeronautics Limited
Operator
India
Wikidata ID
Q1619359