| SLC-1 |
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Air-launched orbital launch vehicle. Family: Air-Launched. Country: USA. Status: Study 2003. Nanosat air-launched orbital vehicle which would be dropped from a boosted F-4 carrier aircraft. The Space Launch Corporation of Irvine, California designed the SLC-1 as an expendable rocket air-launched from an F-4 aircraft. The aircraft's jet engines would be modified using a technology called Mass Injected Pre-Compressor Cooling (MIPCC), where a coolant such as water or liquid oxygen was added to the air at the engine inlet, allowing the engine to operate at higher altitudes than normally possible. The SLC-1 system could launch payloads of 10 to 20 kilograms into LEO for $1 million a launch. The company was seeking funding from the Defense Department to support development of the vehicle when it received the RASCAL contract for a much more elaborate version of the concept from DARPA in 2003. Manufacturer: Space Launch Corporation. LEO Payload: 20 kg (44 lb). to: 185 km Orbit. at: 28.00 degrees. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted. |