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Low cost orbital launch vehicle. Family: LCLV. Country: USA. Status: Design 1988. Other Designations: Aquila. Low-cost hybrid launch vehicle proposed by AMROC in the 1980's. Manufacturer: eAC. LEO Payload: 1,818 kg (4,008 lb). to: 217 km Orbit. Liftoff Thrust: 11,136.700 kN (2,503,630 lbf). Total Mass: 591,180 kg (1,303,320 lb). Core Diameter: 1.83 m (6.00 ft). Total Length: 70.00 m (229.00 ft). Launch Price $: 8.000 million. in: 1987 price dollars. Flyaway Unit Cost $: 19.000 million. in: 1985 unit dollars. - Stage0: 12 x AMROC. Gross Mass: 31,000 kg (68,000 lb). Empty Mass: 5,900 kg (13,000 lb). Motor: 1 x H1500. Thrust (vac): 931.330 kN (209,371 lbf). Isp: 284 sec. Burn time: 75 sec. Length: 19.50 m (63.90 ft). Diameter: 1.83 m (6.00 ft). Propellants: Lox/Solid.
- Stage1: 4 x AMROC. Gross Mass: 31,000 kg (68,000 lb). Empty Mass: 5,900 kg (13,000 lb). Motor: 1 x H1500. Thrust (vac): 931.330 kN (209,371 lbf). Isp: 284 sec. Burn time: 75 sec. Length: 19.50 m (63.90 ft). Diameter: 1.83 m (6.00 ft). Propellants: Lox/Solid.
- Stage2: 2 x AMROC. Gross Mass: 31,000 kg (68,000 lb). Empty Mass: 5,900 kg (13,000 lb). Motor: 1 x H1500. Thrust (vac): 931.330 kN (209,371 lbf). Isp: 284 sec. Burn time: 75 sec. Length: 19.50 m (63.90 ft). Diameter: 1.83 m (6.00 ft). Propellants: Lox/Solid.
- Stage3: 1 x AMROC. Gross Mass: 31,000 kg (68,000 lb). Empty Mass: 5,900 kg (13,000 lb). Motor: 1 x H1500. Thrust (vac): 931.330 kN (209,371 lbf). Isp: 284 sec. Burn time: 75 sec. Length: 19.50 m (63.90 ft). Diameter: 1.83 m (6.00 ft). Propellants: Lox/Solid.
Bibliography:- Interplanetary Spacecraft,
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