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Family: Miscellany. Country: USA. Status: Development 1988. Other Designations: Aquila.
SpecificationsLEO Payload: 1,818 kg. to: 217 km Orbit. Liftoff Thrust: 1,135,630 kgf. Total Mass: 591,180 kg. Core Diameter: 1.8 m. Total Length: 70.0 m. Launch Price $: 8.00 million. in 1987 price dollars. Flyaway Unit Cost $: 19.00 million. in 1985 unit dollars.
- Stage Number: 0. 12 x AMROC Gross Mass: 31,000 kg. Empty Mass: 5,900 kg. Thrust (vac): 94,970 kgf. Isp: 284 sec. Burn time: 75 sec. Isp(sl): 283 sec. Diameter: 1.8 m. Span: 1.8 m. Length: 19.5 m. Propellants: Lox/Solid No Engines: 1. H1500
- Stage Number: 1. 4 x AMROC Gross Mass: 31,000 kg. Empty Mass: 5,900 kg. Thrust (vac): 94,970 kgf. Isp: 284 sec. Burn time: 75 sec. Isp(sl): 283 sec. Diameter: 1.8 m. Span: 1.8 m. Length: 19.5 m. Propellants: Lox/Solid No Engines: 1. H1500
- Stage Number: 2. 2 x AMROC Gross Mass: 31,000 kg. Empty Mass: 5,900 kg. Thrust (vac): 94,970 kgf. Isp: 284 sec. Burn time: 75 sec. Isp(sl): 283 sec. Diameter: 1.8 m. Span: 1.8 m. Length: 19.5 m. Propellants: Lox/Solid No Engines: 1. H1500
- Stage Number: 3. 1 x AMROC Gross Mass: 31,000 kg. Empty Mass: 5,900 kg. Thrust (vac): 94,970 kgf. Isp: 284 sec. Burn time: 75 sec. Isp(sl): 283 sec. Diameter: 1.8 m. Span: 1.8 m. Length: 19.5 m. Propellants: Lox/Solid No Engines: 1. H1500
Bibliography:- 248 - Interplanetary Spacecraft, .
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