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RM-1400
AKA: Asp IV. Status: Retired 1963. Thrust: 12.70 kN (2,855 lbf). Gross mass: 94 kg (207 lb). Unfuelled mass: 27 kg (59 lb). Burn time: 12 s. Height: 2.80 m (9.10 ft). Diameter: 0.17 m (0.54 ft).
Country: USA. Launch Vehicles: Nike Asp, Asp IV, Terrier Asp IV. Propellants: Solid. Stages: RM-1400. Agency: Cooper Development.
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