NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Booster parametric design method for performance and trajectory analysis. part ii- propulsionBooster parametric design method for performance and trajectory analysis - propulsion
Document ID
19640019264
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Verderaime, V. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
June 2, 1964
Subject Category
Propellants
Report/Patent Number
NASA-TM-X-53053
Report Number: NASA-TM-X-53053
Accession Number
64N29178
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PROPULSION
TRAJECTORY
BOOSTER

Related Records

There are no records associated with this record.
No Preview Available