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Altair 2
Part of Altair Family
Thiokol solid rocket engine. Kick stage motor for Delta D, Scout A, Scout X-4. First flight 1963.

AKA: Star 25;TE-M-184-3;X-258. Status: Retired 1973. Number: 29 . Thrust: 22.20 kN (4,991 lbf). Gross mass: 275 kg (606 lb). Unfuelled mass: 37 kg (81 lb). Specific impulse: 266 s. Specific impulse sea level: 242 s. Burn time: 28 s. Height: 2.53 m (8.30 ft). Diameter: 0.64 m (2.09 ft).

Thrust (sl): 20.200 kN (4,541 lbf). Thrust (sl): 2,063 kgf.



Country: USA. Launch Vehicles: Scout A, Scout X-4, Scout X-2B, Thor Delta C, Scout X-4A, Thor Delta D, Thor Delta E, Scout A-1. Propellants: Solid. Stages: Altair 2. Agency: Thiokol.

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