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X-265

Encyclopedia Astronautica
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X-265
Hercules solid rocket engine. Sprint ABM first stage.
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AKA: Sprint ABM-1; Sprint X265. Status: Retired 1992. Gross mass: 4,000 kg (8,800 lb). Burn time: 1.20 s. Height: 3.00 m (9.80 ft). Diameter: 1.37 m (4.49 ft).

Subtopics
Squirt-1 Solid propellant rocket stage.
HIBEX engine Boeing solid rocket engine. HIBEX first stage.
Upstage engine Boeing solid rocket engine. Upstage first stage.
Country: USA. Launch Vehicles: Sprint ABM, HEDI. Propellants: Solid. Stages: X-265. Agency: Hercules.
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