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Space shuttle main engine: Hydraulic systemThe hydraulic actuation system of the space shuttle main engine is discussed. The system consists of five electrohydraulic actuators and a single engine filter used to control the five different propellant valves, which in turn control thrust and mixture ratio of the space shuttle main engine. The hydraulic actuation system provides this control with a precision of 98.7 percent or an error in position no greater than 1.3 percent of full scale rotational travel for critical positions.
Document ID
19810013877
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Geller, G.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Lamb, C. D.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 11, 2013
Publication Date
May 1, 1981
Publication Information
Publication: the 15th Aerospace Mech. Symp.
Subject Category
Spacecraft Propulsion And Power
Accession Number
81N22408
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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