The Wayback Machine - https://web.archive.org/web/20161227202048/http://astronautix.com/i/industriallaunchvehicle.html
Industrial Launch Vehicle

Encyclopedia Astronautica
Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
Industrial Launch Vehicle
Part of AMROC Family
American low cost orbital launch vehicle. Low-cost hybrid launch vehicle proposed by AMROC in the 1980's.
See More

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

  • Stage 0. 12 x AMROC. Gross Mass: 31,000 kg (68,000 lb). Empty Mass: 5,900 kg (13,000 lb). Thrust (vac): 931.330 kN (209,371 lbf). Isp: 284 sec. Burn time: 75 sec. Isp(sl): 283 sec. Diameter: 1.83 m (6.00 ft). Span: 1.83 m (6.00 ft). Length: 19.50 m (63.90 ft). Propellants: Lox/Solid. No Engines: 1. Engine: H1500. Other designations: Aquila. Status: Development 1988.
  • Stage 1. 4 x AMROC. Gross Mass: 31,000 kg (68,000 lb). Empty Mass: 5,900 kg (13,000 lb). Thrust (vac): 931.330 kN (209,371 lbf). Isp: 284 sec. Burn time: 75 sec. Isp(sl): 283 sec. Diameter: 1.83 m (6.00 ft). Span: 1.83 m (6.00 ft). Length: 19.50 m (63.90 ft). Propellants: Lox/Solid. No Engines: 1. Engine: H1500. Other designations: Aquila. Status: Development 1988.
  • Stage 2. 2 x AMROC. Gross Mass: 31,000 kg (68,000 lb). Empty Mass: 5,900 kg (13,000 lb). Thrust (vac): 931.330 kN (209,371 lbf). Isp: 284 sec. Burn time: 75 sec. Isp(sl): 283 sec. Diameter: 1.83 m (6.00 ft). Span: 1.83 m (6.00 ft). Length: 19.50 m (63.90 ft). Propellants: Lox/Solid. No Engines: 1. Engine: H1500. Other designations: Aquila. Status: Development 1988.
  • Stage 3. 1 x AMROC. Gross Mass: 31,000 kg (68,000 lb). Empty Mass: 5,900 kg (13,000 lb). Thrust (vac): 931.330 kN (209,371 lbf). Isp: 284 sec. Burn time: 75 sec. Isp(sl): 283 sec. Diameter: 1.83 m (6.00 ft). Span: 1.83 m (6.00 ft). Length: 19.50 m (63.90 ft). Propellants: Lox/Solid. No Engines: 1. Engine: H1500. Other designations: Aquila. Status: Development 1988.

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

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
� 1997-2016 Mark Wade - Contact
� / Conditions for Use