As an alternative to magnetic propulsion for launch assist, the authors propose a pneumatic launch assist system. Using off-the-shelf components, coupled with familiar steel and concrete construction, a launch assist system can be brought from the initial feasibility stage, through a flight capable 5000 kg demonstrator to a deployed full size launch assist system in 10 years. The final system would be capable of accelerating a 450,000 kg vehicle to 270 ms−1. The CELT system uses commercially available compressors and valves to build a fail-safe system in less than half the time of a full Mag-Lev (magnetic levitation) system, and at a small fraction of the development cost. The resulting system could be ready in time to support some Gen 2 (Generation 2) vehicles, as well as the proposed Gen 3 vehicle.
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2 February 2001
Space Technology and Applications International Forum - 2001
11-14 Feb 2001
Albuquerque, New Mexico
Research Article|
February 02 2001
Closed end launch tube (CELT) Available to Purchase
Dale E. Lueck;
Dale E. Lueck
NASA/KSC, Spaceport Engineering and Technology Directorate, YA-D2, John F. Kennedy Space Center, Florida 32899
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Clyde F. Parrish
Clyde F. Parrish
NASA/KSC, Spaceport Engineering and Technology Directorate, YA-D2, John F. Kennedy Space Center, Florida 32899
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Dale E. Lueck
Clyde F. Parrish
NASA/KSC, Spaceport Engineering and Technology Directorate, YA-D2, John F. Kennedy Space Center, Florida 32899
AIP Conf. Proc. 552, 660–664 (2001)
Citation
Dale E. Lueck, Clyde F. Parrish; Closed end launch tube (CELT). AIP Conf. Proc. 2 February 2001; 552 (1): 660–664. https://doi.org/10.1063/1.1357990
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