Hyperion-1

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Hyperion-1

Solid rocket stage. 6.00 kN (1,349 lbf) thrust. Mass 100 kg (220 lb).

Status: Retired 1997. Thrust: 6.00 kN (1,349 lbf). Gross mass: 100 kg (220 lb). Unfuelled mass: 46 kg (101 lb). Burn time: 15 s. Height: 5.80 m (19.00 ft). Diameter: 0.15 m (0.49 ft).

Country: USA. Engines: Hyperion engine. Launch Vehicles: Hyperion. Propellants: Solid. Agency: eAc.

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