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Pegasus XL-2
Part of Orion 50 Family
Hercules solid rocket engine. Used on Pegasus XL launch vehicle. First flight 1994.

Status: Active. Number: 33 . Thrust: 153.50 kN (34,508 lbf). Gross mass: 4,331 kg (9,548 lb). Unfuelled mass: 416 kg (917 lb). Specific impulse: 290 s. Specific impulse sea level: 240 s. Burn time: 73 s. Height: 3.58 m (11.74 ft). Diameter: 1.27 m (4.16 ft).

Thrust (sl): 127.000 kN (28,550 lbf). Thrust (sl): 12,954 kgf. Chamber Pressure: 58.00 bar. Area Ratio: 65.



Country: USA. Launch Vehicles: Pegasus XL, Pegasus XL/HAPS, Minotaur 1, Minotaur 2. Propellants: Solid. Stages: Pegasus XL-2. Agency: Hercules.

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