 By July 2002, Turbomeca was ready to launch the 900 kW (1,200 hp) engine development with HAL for 11% for the ALH, then renamed Dhruv.The TM333 was derated from for the Dhruv, and the Ardiden 1H "Shakti" would be derated from .The Ardiden 1A was designed to for the Eurocopter EC155HP+, and the Ardiden 2K for the Agusta-Bell AB.139.