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Pegasus-2
Part of Orion 50
Hercules solid rocket engine. Used on Pegasus, Taurus. First flight 1989.
AKA: Orion 50. Status: Active. Number: 19 . Thrust: 118.20 kN (26,572 lbf). Gross mass: 3,370 kg (7,420 lb). Unfuelled mass: 345 kg (760 lb). Specific impulse: 290 s. Burn time: 74 s. Height: 2.65 m (8.69 ft). Diameter: 1.27 m (4.16 ft).
Thrust (sl): 97.100 kN (21,829 lbf). Thrust (sl): 9,907 kgf. Chamber Pressure: 58.00 bar. Area Ratio: 65.
Country:
USA.
Launch Vehicles:
Pegasus,
Pegasus/HAPS,
Taurus,
ARPA Taurus,
Pegasus H,
Taurus 2210,
Taurus 2110,
GBI,
Taurus 3210,
Taurus 3110.
Propellants:
Solid.
Stages:
Pegasus-2.
Agency:
Hercules.
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