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Altair 1
Part of Altair
Thiokol solid rocket engine. Used on Atlas Able, Blue Scout 2, Caleb, Delta, Delta A, Delta B, Delta C. First flight 1959.
AKA: Caleb-2;X-248. Status: Retired 1962. Number: 51 . Thrust: 12.40 kN (2,788 lbf). Gross mass: 238 kg (524 lb). Unfuelled mass: 30 kg (66 lb). Specific impulse: 256 s. Specific impulse sea level: 233 s. Burn time: 38 s. Height: 1.83 m (6.00 ft). Diameter: 0.46 m (1.50 ft).
Thrust (sl): 11.300 kN (2,540 lbf). Thrust (sl): 1,156 kgf.
Country:
USA.
Launch Vehicles:
Atlas Able,
Delta,
Bold Orion 2,
Thor Delta A,
Javelin,
Thor Able III,
Atlas C Able,
Shotput,
Atlas D Able,
Thor Able II M1,
Thor Able IV,
Scout X,
Thor Delta,
Scout X-1,
Caleb,
Journeyman,
Blue Scout II,
Trailblazer 2,
Scout X-2,
Scout X-3A,
Thor Delta B,
Scout X-3,
Thor Delta C1,
Scanner,
Delta C.
Propellants:
Solid.
Stages:
Altair 1.
Agency:
Thiokol.
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