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Industrial Launch Vehicle
Part of AMROC
American low cost orbital launch vehicle. Low-cost hybrid launch vehicle proposed by AMROC in the 1980's.

AKA: Aquila. Status: Design 1988. Payload: 1,818 kg (4,008 lb). Thrust: 11,136.70 kN (2,503,630 lbf). Gross mass: 591,180 kg (1,303,320 lb). Height: 70.00 m (229.00 ft). Diameter: 1.83 m (6.00 ft). Apogee: 217 km (134 mi).

LEO Payload: 1,818 kg (4,008 lb) to a 217 km orbit. Launch Price $: 19.000 million in 1987 dollars.

Stage Data - Industrial Launch Vehicle



Family: LCLVs, low cost, orbital launch vehicle. Country: USA. Engines: H1500. Stages: AMROC Aquila. Agency: eAc. Bibliography: 248.

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