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Development and test of electromechanical actuators for thrust vector controlA road map of milestones toward the goal of a full scale Redesigned Solid Rocket Motor/Flight Support Motor (RSRM/FSM) hot fire test is discussed. These milestones include: component feasibility, full power system demonstration, SSME hot fire tests, and RSRM hot fire tests. The participation of the Marshall Space Flight Center is emphasized.
Document ID
19930066209
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Weir, Rae A. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Cowan, John R. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 16, 2013
Publication Date
June 1, 1993
Subject Category
Mechanical Engineering
Report/Patent Number
AIAA PAPER 93-2458
Meeting Information
Meeting: AIAA, SAE, ASME, and ASEE, Joint Propulsion Conference and Exhibit
Location: Monterey, CA
Country: United States
Start Date: June 28, 1993
End Date: June 30, 1993
Sponsors: ASME, SAE, AIAA, ASEE
Accession Number
93A50206
Distribution Limits
Public
Copyright
Other

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