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Pegasus-4
Hydrazine propellant rocket stage. .

Status: Retired 1994. Thrust: 666 N (149 lbf). Gross mass: 90 kg (198 lb). Unfuelled mass: 17 kg (37 lb). Specific impulse: 236 s. Burn time: 241 s. Height: 0.25 m (0.82 ft). Diameter: 0.97 m (3.18 ft). Span: 0.97 m (3.18 ft).

Cost $ : 0.100 million. No Engines: 3.



Country: USA. Engines: MR-107. Launch Vehicles: Pegasus/HAPS.

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