Kaveri Dry Engine Records 48.5 kN Peak Thrust in High-Altitude and Flight Trials
India's Kaveri dry engine, also called the Kaveri Derivative Engine, recorded a peak dry thrust of 48.5 kilonewtons during high-altitude and flight trials in Russia in September 2026, above its target of about 46 kN. Developed by DRDO's Gas Turbine Research Establishment, Bengaluru, the non-afterburning turbofan is intended for the Ghatak stealth Unmanned Combat Aerial Vehicle. Trials were held at the Central Institute of Aviation Motors and the Gromov Flight Research Institute using a modified Ilyushin Il-76 flying testbed. The Ministry of Defence targets certification in 2026 by CEMILAC. Kaveri 2.0 is planned at 55-60 kN dry and 90-100 kN with afterburner.
Dry thrust is engine thrust without afterburner use; an afterburner raises thrust by injecting fuel into the exhaust stream | The non-afterburning Kaveri engine was cleared for in-flight testing on 23 December 2024 | CEMILAC, the Centre for Military Airworthiness and Certification, grants airworthiness clearance in Indian military aviation