Status: Retired 1971. First Launch: 1970-01-01. Last Launch: 1971-10-09. Number: 2 . Thrust: 8.40 kN (1,888 lbf). Gross mass: 20 kg (44 lb). Unfuelled mass: 11 kg (24 lb). Burn time: 2.90 s. Height: 2.50 m (8.20 ft). Diameter: 0.12 m (0.39 ft). Apogee: 20 km (12 mi).
RH-125S ISRO VSSC solid rocket engine. Menaka II second stage. |