Aquarius (rocket)

Aquarius was a low-cost launch vehicle concept designed by Space Systems/Loral to carry small, inexpensive payloads into LEO.

Aquarius
FunctionSSTO Expendable launch system
ManufacturerSpace Systems/Loral, Aerojet, Microcosm
Country of originUnited States
Size
Height43.00 m (141.08 ft)
Diameter4 m (13 ft)
Mass130,000 kg (290,000 lb) (10,000 kg (22,000 lb) empty)
Stages1
Capacity
Payload to LEO1,000 kg (2,200 lb) to a 200 km orbit
Launch history
StatusCancelled
Launch sitesHawaii
Total launches0
stage
Engines1
Thrust400,000 lbf (1.8 MN)
FuelLOX/LH2

Concept

The vehicle was primarily intended for launching bulk products, like water, fuel, and other consumables, that are inexpensive to replace in the event of a launch failure. The target launch cost was $1 million. Aquarius was designed to be a single-stage vehicle 43 meters (141 ft) high and 4 meters (13.1 ft) in diameter and powered by a single pressure fed engine using liquid hydrogen and oxygen propellants stored in a composite pressure tank.[1] Launch would have taken place from a floating position in the ocean to minimize launch infrastructure with the ability to place a 1,000-kilogram (2,200 lb) payload into a 200-kilometer (120 mi), 52-degree orbit. The payload, located in the base of the vehicle, would be extracted by an orbiting space tug for transfer to its ultimate destination, like the ISS or a propellant depot, after which the vehicle would de-orbit and be destroyed.[2]

Vortex Cooled Chamber Wall Engine

Space Systems/Loral teamed with Microcosm, and Wilson Composite Technologies to study Aquarius under a $110,000 grant awarded by the state of California in April 2001 and delivered a final report in June 2002. Funding of $1 million was provided in the FY 2004 Defense Appropriations Act to develop a prototype of the low-cost engine for the vehicle. The engine would provide 400,000 pounds-force (1.8 MN) of thrust using liquid oxygen and liquid hydrogen as propellants. For the engine development, Space Systems/Loral is partnered with Aerojet, ORBITEC and Microcosm, under the auspices of the Air Force Research Laboratory and was completed in 2006.[3][4] It confirmed that an ORBITEC engine design with inherently low cost can be scaled up to an intermediate thrust level, from which the next scale-up step to Aquarius should be achievable. [5][6]

COTS bid

The proposal made with Constellation Services International for Commercial Orbital Transportation Services in 2006 was not selected.[7]$150 million was the planned development cost, as part of a $700 million project (that included a space tug). 100 launches per year were needed to be profitable. One third of the launches were by design allowed to fail. Target costs were $1 million per launch or $1000/kg to LEO.[1]

gollark: - lampshades
gollark: - hexagon (geometry)
gollark: - mossy cobblestone
gollark: - spears
gollark: - spheres

See also

References
  1. "aquarius". astronautix.com. Archived from the original on November 12, 2011. Retrieved February 13, 2012.
  2. Andrew E. Turner (January 30, 2006). "Low-cost launch and orbital depots: the Aquarius system". thespacereview.com.
  3. Andrew E. Turner, Aaron Leichner (2006-10-24). "Hydrogen Pressurization of LOX: High Risk/High Reward" (PDF). dtic.mil.
  4. Andrew E. Turner (2005). "AQUARIUS LOW COST LAUNCH MAIN ENGINE STUDY" (PDF). AIAA. responsivespace.com. p. 24. Archived from the original (PDF) on 2006-05-16.
  5. "2004 U.S. COMMERCIAL SPACE TRANSPORTATION DEVELOPMENTS AND CONCEPTS: VEHICLES, TECHNOLOGIES, AND SPACEPORTS" (PDF). Commercial Space Transportation Office. p. 15.
  6. Andrew W. Turner ; William H. Knuth (March–April 2006). "The Vortex Cooled Chamber Wall Engine: A Tamed Tornado". SPACE TIMES Magazine.
  7. "Space Systems/Loral Proposes Bus for NASA's Cargo Needs" (Press release). Space News. 2007-12-10. Archived from the original on 12 December 2007. Retrieved 2007-12-10.
  • Space Time magazine, May/June 2001
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