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Space Shuttle system solid rocket booster.Description of the mission and systems requirement of the solid rocket booster as it supports the Shuttle vehicle configuration. The solid booster is equipped with load skirts and linkages that can accommodate full mission loads, a solid propellant motor for delivering required performance, thrust vector control for augmentation of Shuttle vehicle ascent control, staging and separation systems, and electrical subsystems. To recover and reuse the solid booster case a recovery package is provided. The definition of these functional elements of the solid booster are discussed with the requirements placed on each element to satisfy the overall booster objective.
Document ID
19730051284
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Thomason, H. E.
(NASA Marshall Space Flight Center Huntsville, Ala., United States)
Date Acquired
August 7, 2013
Publication Date
July 1, 1973
Subject Category
Space Vehicles
Report/Patent Number
AIAA PAPER 73-606
Report Number: AIAA PAPER 73-606
Meeting Information
Meeting: Joint Space Mission Planning and Execution Meeting
Location: Denver, CO
Start Date: July 10, 1973
End Date: July 12, 1973
Sponsors: AIAA, ASME, SAE
Accession Number
73A36086
Distribution Limits
Public
Copyright
Other

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