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Space shuttle rudder/speedbrake actuation subsystemThe Rudder/Speedbrake (R/SB) Actuation Subsystem for use on the NASA Space Shuttle Orbiter is an electro-hydro-mechanical system which provides the control and positionary capability of the orbiter aero-dynamic primary flight control surface. The system is located in the vehicle's vertical stabilizer. The geared rotary actuators provide a power hinge feature of the split panel rudder. Actuation of both panels in the same direction provides conventional rudder control; actuating the panels differentially provides a speedbrake function intended to control both speed and pitch. The commands may be superimposed on one another. The system consists of one power drive unit which responds to quadredundant avionic signals to generate a rotary output, four geared rotary actuators, which develop rotary position and torque as outputs, and ten torque transmitting drive-shifts.
Document ID
19850008656
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Naber, R. A.
(Sundstrand Advanced Technology Group Rockford, IL, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Publication Information
Publication: NASA. Johnson Space Center Space Shuttle Tech. Conf., Pt. 2
Subject Category
Space Transportation
Accession Number
85N16965
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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