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RH-125S
Part of RH-125
ISRO VSSC solid rocket engine. Menaka II second stage.

AKA: Menaka II-2. Status: Retired 1977. Thrust: 1.30 kN (292 lbf). Gross mass: 20 kg (44 lb). Unfuelled mass: 14 kg (30 lb). Burn time: 32 s. Height: 1.60 m (5.20 ft). Diameter: 0.12 m (0.39 ft).

Country: India. Launch Vehicles: Menaka II. Propellants: Solid. Stages: RH-125S. Agency: ISRO.
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