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RM-1100
Part of Asp II engine
Cooper solid rocket engine.

AKA: Asp. Status: Retired 1963. Thrust: 26.00 kN (5,845 lbf). Gross mass: 100 kg (220 lb). Unfuelled mass: 18 kg (39 lb). Burn time: 5.30 s. Height: 2.70 m (8.80 ft). Diameter: 0.17 m (0.54 ft).

Country: USA. Launch Vehicles: Asp, ASCAMP, Terrier Asp, Astrobee 500, Asp Apache. Propellants: Solid. Stages: RM-1100. Agency: Cooper Development.
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