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AMROC Aquila
LOx/Solid propellant rocket stage. .

AKA: AMROC;Aquila. Status: Design 1988. Thrust: 931.33 kN (209,371 lbf). Gross mass: 31,000 kg (68,000 lb). Unfuelled mass: 5,900 kg (13,000 lb). Specific impulse: 284 s. Specific impulse sea level: 283 s. Burn time: 75 s. Height: 19.50 m (63.90 ft). Diameter: 1.83 m (6.00 ft). Span: 1.83 m (6.00 ft).

Cost $ : 1.000 million.



Country: USA. Engines: H1500. Launch Vehicles: Industrial Launch Vehicle. Propellants: Lox/Solid.

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