Castor 1

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Castor 1

Part of Castor

Castor 1

Thiokol solid rocket engine. Used as apogee kick motor on Delta D, LT Thor Agena D, Scout X-1, Scout X-2, Scout X-3, Scout X-4, TA Thor Agena B, TA Thor Agena D. First flight 1960. M33-20 fourth stage.

AKA: M33-20-4. Status: Active. Number: 141 . Thrust: 286.00 kN (64,295 lbf). Gross mass: 3,852 kg (8,492 lb). Unfuelled mass: 535 kg (1,179 lb). Specific impulse: 247 s. Specific impulse sea level: 232 s. Burn time: 27 s. Height: 5.92 m (19.42 ft). Diameter: 0.79 m (2.59 ft).

Thrust (sl): 268.600 kN (60,384 lbf). Thrust (sl): 27,393 kgf.

More at: Castor 1.

Country: USA. Launch Vehicles: Little Joe 1 4C, Scout X, Scout X-1, Blue Scout Jr, RAM A, Trailblazer 2, Scout X-1A, Scout X-2, Scout X-2M, Scout X-3A, RAM B, Castor-Recruit, ARPAT, Scout X-3, Blue Scout Jr SLV-1B(m), Scout X-2 1C, Scout X-3M, Thor SLV-2A Agena D, Scout X-4, Thor SLV-2A Agena B, Scout X-2B, Athena RTV, Scout X-4A, Thor Delta D, Scout X-3C, Thor Delta E, Thorad SLV-2G Agena D, Strypi IV, Thor Delta G, Castor, Strypi VI, Thorad SLV-2H Agena D, Strypi, Castor Lance, Super Chief II, Strypi IIR, Strypi VIIR, Talos Castor, DOT, Strypi XI, Castor 4A, Strypi IX, Strypi Tomahawk. Propellants: Solid. Stages: Castor 1. Agency: Thiokol.

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