Castor 2

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Castor 2

Part of Castor

Thiokol solid rocket engine. Used in Scout A; Delta E; H-1-0; Castor 2. License built in Japan for H-1. First flight 1960. Solid propellant rocket stage. Version for Japanese H-1 booster.

AKA: H-1-0;TX-354-3. Status: In Production. Number: 1054 . Thrust: 258.90 kN (58,203 lbf). Gross mass: 4,424 kg (9,753 lb). Unfuelled mass: 695 kg (1,532 lb). Specific impulse: 262 s. Specific impulse sea level: 232 s. Burn time: 37 s. Height: 6.04 m (19.81 ft). Diameter: 0.79 m (2.59 ft).

Thrust (sl): 229.300 kN (51,549 lbf). Thrust (sl): 23,379 kgf. Area Ratio: 7.45.

Country: USA. Launch Vehicles: Scout A, Blue Scout Junior, Blue Scout I, Blue Scout II, Blue Scout Jr SLV-1C, Scout B, Thor Delta E, Scout B 2A, Thor Delta E1, Scout X-5C, Thor Delta J, Thor Delta N, Thor Delta M, Thorad SLV-2H Agena D, Thor Delta L, Thor Delta N6, Thor Delta M6, Scout B-1, Scout B-1 F, Delta 0900, Scout D-1, Delta 1604, Delta 0300, Strypi VIIAR, Delta 1914, Scout D-1 F, Delta 1913, Scout A-1, Delta 1900, Delta 2313, Strypi IIAR, Delta 2914, Scout E-1, Delta 2310, Delta 2910, Delta 1410, Scout F-1, Delta 1910, Delta 2913, N-1, Scout G-1, N-2, N-2 (2), Delta 0100, Scout D, H-1, H-1 (2), H-1 6R, Advanced Scout. Propellants: Solid. Stages: Castor 2. Agency: Thiokol.

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