Solid rocket booster thrust vector control subsystem test report (D-1)

Published 2019-06-20 From Legacy CDMS 1 author

Attribution

This is the abstract and citation. Full text lives at NASA NTRS — we link out rather than host. All credit to the authors and Legacy CDMS.

Abstract

Verbatim from NASA NTRS. Not paraphrased, not summarized.

The results of the sequence of tests performed on the space shuttle solid rocket booster thrust vector control subsystem are presented. The operational characteristics of the thrust vector control subsystem components, as determined from the tests, are discussed. Special analyses of fuel consumption, basic steady state characteristics, GN2 spin, and actuator displacement were reviewed which will aid in understanding the performance of the auxiliary power unit. The possibility of components malfunction is also discussed.

Author

Pagan, B. NASA Marshall Space Flight Center

Citation: Pagan, B. (2019). Solid rocket booster thrust vector control subsystem test report (D-1). Legacy CDMS. NASA NTRS ID 19780017185. https://ntrs.nasa.gov/citations/19780017185 ↗