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Design of Electrical Systems for Rocket Propulsion Test Facilities at the John C. Stennis Space CenterThis viewgraph presentation reviews the design of the electrical systems that are required for the testing of rockets at the Rocket Propulsion Facility at NASA Stennis Space Center (NASA SSC). NASA/SSC s Mission in Rocket Propulsion Testing Is to Acquire Test Performance Data for Verification, Validation and Qualification of Propulsion Systems Hardware. These must be accurate reliable comprehensive and timely. Data acquisition in a rocket propulsion test environment is challenging: severe temporal transient dynamic environments, large thermal gradients, vacuum to 15 ksi pressure regimes SSC has developed and employs DAS, control systems and control systems and robust instrumentation that effectively satisfies these challenges.
Document ID
20070012331
Acquisition Source
Stennis Space Center
Document Type
Conference Paper
Authors
Hughes, Mark S.
(NASA Stennis Space Center Stennis Space Center, MS, United States)
Davis, Dawn M.
(NASA Stennis Space Center Stennis Space Center, MS, United States)
Bakker, Henry J.
(NASA Stennis Space Center Stennis Space Center, MS, United States)
Jensen, Scott L.
(NASA Stennis Space Center Stennis Space Center, MS, United States)
Date Acquired
August 23, 2013
Publication Date
January 1, 2007
Subject Category
Electronics And Electrical Engineering
Report/Patent Number
SPPT-8075-0001-ELEC
Meeting Information
Meeting: Mississippi Engineering Society
Location: Jackson, MS
Country: United States
Start Date: February 25, 2007
End Date: February 27, 2007
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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