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Quarter Scale RLV Multi-Lobe LH2 Tank Test ProgramThirty cryogenic pressure cycles have been completed on the Lockheed Martin Michoud Space Systems quarter scale RLV composite multi-lobe liquid hydrogen propellant tank assembly, completing the initial phases of testing and demonstrating technologies key to the success of large scale composite cryogenic tankage for X33, RLV, and other future launch vehicles.
Document ID
19980237338
Acquisition Source
Marshall Space Flight Center
Document Type
Other
Authors
Blum, Celia (Lockheed Martin Michoud Space Systems New Orleans, LA United States)
Puissegur, Dennis (Lockheed Martin Michoud Space Systems New Orleans, LA United States)
Tidwell, Zeb (Lockheed Martin Tactical Aircraft Systems Fort Worth, TX United States)
Webber, Carol (Lockheed Martin Space Mission Systems and Services Houston, TX United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1998
Subject Category
Structural Mechanics
Funding Number(s)
CONTRACT_GRANT: NCC8-115
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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