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Altair 2
Part of Altair
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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