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Antares 2
Part of Antares
Thiokol solid rocket engine. Used on Scout A, Scout B, Scout D, Scout F, Scout X-2, Scout X-3, Scout X-4. First flight 1962.
AKA: X-259. Status: Retired 1995. Number: 92 . Thrust: 93.10 kN (20,930 lbf). Gross mass: 1,400 kg (3,000 lb). Unfuelled mass: 300 kg (660 lb). Specific impulse: 293 s. Specific impulse sea level: 233 s. Burn time: 36 s. Height: 2.90 m (9.50 ft). Diameter: 0.78 m (2.55 ft).
Thrust (sl): 74.000 kN (16,635 lbf). Thrust (sl): 7,549 kgf.
Country:
USA.
Launch Vehicles:
Scout A,
Scout X-2,
Scout X-2M,
Scout X-3A,
Scout X-3,
Scout X-2 1C,
Scout X-3M,
Scout X-4,
Scout X-2B,
Scout X-4A,
Scout X-3C,
Scout B,
Scout B 2A,
SPARTA,
Scout X-5C,
Athena H,
Scout B-1,
Scout B-1 F,
Scout D-1,
Scout D-1 F,
Scout A-1,
Scout E-1,
Scout F-1,
Scout D,
Strypi XI,
Strypi IX,
Strypi Tomahawk.
Propellants:
Solid.
Stages:
Antares 2.
Agency:
Thiokol.
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