Liquid oxygen propellant densification production and performance test results with a large-scale flight-weight propellant tank for the X33 RLV /

Bibliographic Details

Main Author:	Tomsik, Thomas M.
Corporate Author:	NASA Glenn Research Center
Other Authors:	Meyer, Michael L.
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2010]
Series:	NASA technical memorandum ; 216247.
Subjects:	Liquid oxygen. Propellants. Densification. Cryogenics. Oxygen production. Performance tests. Propellant tanks. X-33 reusable launch vehicle.
Online Access:	https://purl.fdlp.gov/GPO/gpo3599