Algol 2

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Algol 2

Part of Algol

CSD solid rocket engine. Used on Scout A, Scout B, Scout X-3, Scout X-4; proposed as strap-on for Titan 3BAS2. First flight 1962.

Status: First flight 1962. Number: 67 . Thrust: 564.20 kN (126,837 lbf). Gross mass: 11,600 kg (25,500 lb). Unfuelled mass: 1,650 kg (3,630 lb). Specific impulse: 255 s. Specific impulse sea level: 232 s. Burn time: 47 s. Height: 9.09 m (29.82 ft). Diameter: 1.01 m (3.31 ft).

Thrust (sl): 513.300 kN (115,394 lbf). Thrust (sl): 52,347 kgf.

Country: USA. Launch Vehicles: Scout A, Titan 3BAS2, Scout X-3A, Scout X-3, Scout X-3M, Scout X-4, Scout X-4A, Scout X-3C, Scout B, Scout B 2A, Scout B-1, Scout A-1. Propellants: Solid. Stages: Algol 2. Agency: CSD.

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