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Engine Model: RH-125. Designer: ISRO VSSC. Gross Mass: 20 kg (44 lb). Empty Mass: 11 kg (24 lb). Propellants: Solid. Thrust(vac): 8.400 kN (1,888 lbf). Burn time: 2.90 sec. Diameter: 0.12 m (0.39 ft). Length: 1.40 m (4.50 ft). Country: India.
Engine Model: RH-125S. Designer: ISRO VSSC. Gross Mass: 20 kg (44 lb). Empty Mass: 14 kg (30 lb). Propellants: Solid. Thrust(vac): 1.300 kN (292 lbf). Burn time: 32 sec. Diameter: 0.12 m (0.39 ft). Length: 1.60 m (5.20 ft). Country: India.
RH-125 used on Rocket Stages - Used on stage: RH-125. on launch vehicle: RH.
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