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Space shuttle launch vehicle performance trajectory, exchange ratios, and dispersion analysis

Author
Lott, L. N.
Published
Mar 1, 1973.
Physical Description
1 electronic document
Additional Creators
Blackwell, D. L. and Toelle, R. G.
Online Version

Availability

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
A 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.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19750012374.
Accession ID: 75N20446.
NASA-TM-X-64918.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15740546