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Liquid Rocket Engine Testing OverviewContents include the following: Objectives and motivation for testing. Technology, Research and Development Test and Evaluation (RDT&E), evolutionary. Representative Liquid Rocket Engine (LRE) test compaigns. Apollo, shuttle, Expandable Launch Vehicles (ELV) propulsion. Overview of test facilities for liquid rocket engines. Boost, upper stage (sea-level and altitude). Statistics (historical) of Liquid Rocket Engine Testing. LOX/LH, LOX/RP, other development. Test project enablers: engineering tools, operations, processes, infrastructure.
Document ID
20050182932
Acquisition Source
Stennis Space Center
Document Type
Preprint (Draft being sent to journal)
Authors
Rahman, Shamim (NASA Stennis Space Center Stennis Space Center, MS, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2005
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
SSTI-2200-0047
Report Number: SSTI-2200-0047
Meeting Information
Meeting: AIAA Short Course on Liquid Rocket Engine Testing
Location: Tucson, AZ
Country: United States
Start Date: July 13, 2005
End Date: July 14, 2005
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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