Thrust vector control for the Space Shuttle Solid Rocket MotorThrust vector control (TVC) for the Space Shuttle Solid Rocket Motor (SRM) is obtained by omniaxis vectoring of the nozzle. The development and integration of the system are under the cognizance of Marshall Space Flight Center (MSFC). The nozzle and flexible bearing have been designed and will be built by Thiokol Corporation/Wasatch Division. The vector requirements of the system, the impact of multiple reuse on the components, and the unique problems associated with a large flexible bearing are discussed. The design details of each of the major TVC subcomponents are delineated. The subscale bearing development program and the overall development schedule also are presented.
Document ID
19750061533
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Counter, D. N. (NASA Marshall Space Flight Center Huntsville, Ala., United States)
Brinton, B. C. (Thiokol Corp. Brigham City, Utah, United States)