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Study of solid rocket motor for space shuttle booster, volume 2, book 3, appendix A.

Published
Mar 15, 1972.
Physical Description
1 electronic document
Online Version

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
A systems requirements analysis for the solid propellant rocket engine to be used with the space shuttle was conducted. The systems analysis was developed to define the physical and functional requirements for the systems and subsystems. The operations analysis was performed to identify the requirements of the various launch operations, mission operations, ground operations, and logistic and flight support concepts.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19730016072.
Accession ID: 73N24799.
TWR-5672-VOL-2-BK-3-APP-A.
NASA-CR-123728.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15748977