| RH-125 |
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Model: RH-200-2. Gross Mass: 20 kg (44 lb). Empty Mass: 11 kg (24 lb). Thrust (vac): 8.400 kN (1,888 lbf). Burn time: 2.90 sec. Propellants: Solid. Diameter: 0.12 m (0.39 ft). Length: 1.40 m (4.50 ft). Country: India. No Engines: 1. Motor: RH-125. Status: Active. First Flight: 1970. Last Flight: 2008. No Launched: 808. Used as: RH-125. Release conditions: ISRO VSSC.
Model: Menaka II-2. Gross Mass: 20 kg (44 lb). Empty Mass: 14 kg (30 lb). Thrust (vac): 1.300 kN (292 lbf). Burn time: 32 sec. Propellants: Solid. Diameter: 0.12 m (0.39 ft). Length: 1.60 m (5.20 ft). Country: India. No Engines: 1. Motor: RH-125S. Status: Retired 1977. First Flight: 1970. Last Flight: 1977. No Launched: 3. Used as: RH-125. Release conditions: ISRO VSSC.
Used on Launch Vehicles:
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