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RM-3141
GCR solid rocket engine. Jaguar third stage.

AKA: Jaguar-3. Status: Retired 1961. Thrust: 8.60 kN (1,933 lbf). Gross mass: 25 kg (55 lb). Unfuelled mass: 4.00 kg (8.80 lb). Burn time: 7.60 s. Height: 1.20 m (3.90 ft). Diameter: 0.15 m (0.49 ft).



Country: USA. Launch Vehicles: ASCAMP, Strongarm, Jaguar B-57. Propellants: Solid. Stages: RM-3141. Agency: JPL, GCR.

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