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Closed End Launch Tube (CELT)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 meters per second. 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.
Document ID
20010027422
Acquisition Source
Kennedy Space Center
Document Type
Preprint (Draft being sent to journal)
Authors
Lueck, Dale E.
(NASA Kennedy Space Center Cocoa Beach, FL United States)
Parrish, Clyde F.
(NASA Kennedy Space Center Cocoa Beach, FL United States)
Delgado, H.
Date Acquired
September 7, 2013
Publication Date
January 1, 2000
Subject Category
Launch Vehicles And Launch Operations
Meeting Information
Meeting: Space Technology and International Forum
Location: Albuquerque, NM
Country: United States
Start Date: February 11, 2001
End Date: February 14, 2001
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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