NASA NTRS · 19930066209
Development and test of electromechanical actuators for thrust vector control
Abstract
A 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.
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Weir, Rae A., Cowan, John R.. 1993-06-01. Development and test of electromechanical actuators for thrust vector control. https://ntrs.nasa.gov/citations/19930066209
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