The successful static testing of the fourth Space Shuttle Solid Rocket Motor (SRM) is described. Transportation and support equipment concepts and component reusability are demonstrated. The evolution of the SRM transportation support equipment and special test equipment designs are reviewed, and development activities are discussed. Handling and processing aspects of large, heavy components are reviewed briefly.
Space shuttle SRM development
01.03.1979
Sonstige
Keine Angabe
Englisch
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