Space structures technology for future flight systems
Explore the source record for details and available documents.
SEARCH · Engineering Papers
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Explore the source record for details and available documents.
Explore the source record for details and available documents.
presents the development of a new type of ultra-lightweight space boom, called the self-deployable Spring Strip Boom or simply the S cubed boom. It describes the fundamental design concept and several variations of design configurations. Test results of proof of concept models are discussed and compared with results obtained by analytical simultations.
This paper describes the concept and development of a new type of space inflatable/rigidizable structures, called the spring-tape-reinforced alluminum laminate booms (simply, STR booms).
Deployable and inflatable structures are successfully used in a wide variety of earth-bound applications. Their use in space, however, requires not only assurance that the structure will survive a launch to space, but also certainly that the desired deployed configuration and that the processes of deployment, inflation and rigidization in space will be successful and without posing a threat to the hosting satellite or vessel.