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
Space shuttle launch vehicle performance trajectory, exchange ratios, and dispersion analysisA baseline space shuttle performance trajectory for Mission 3A launched from WTR has been generated. Design constraints of maximum dynamic pressure, longitudinal acceleration, and delivered payload were satisfied. Payload exchange ratios are presented with explanation on use. Design envelopes of dynamic pressure, SRB staging point, aerodynamic heating and flight performance reserves are calculated and included.
Document ID
19750012374
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Toelle, R. G. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Blackwell, D. L. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Lott, L. N. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1973
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-TM-X-64918
Report Number: NASA-TM-X-64918
Accession Number
75N20446
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

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