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Asp II engine
Cooper solid rocket engine. Asp III 4L first stage.

AKA: Asp II;Asp III 4L-1. Status: Retired 1959. Number: 1 . Thrust: 26.00 kN (5,845 lbf). Gross mass: 100 kg (220 lb). Unfuelled mass: 18 kg (39 lb). Burn time: 3.60 s. Height: 2.70 m (8.80 ft). Diameter: 0.17 m (0.54 ft).

Subtopics
RM-1100 Cooper solid rocket engine.
RM-1400 Cooper solid rocket engine.
Country: USA. Launch Vehicles: Asp III, Asp II. Propellants: Solid. Stages: Asp II engine. Agency: Cooper Development.
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