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Hot Fire Ignition Test with Densified Liquid Hydrogen using a RL10B-2 Cryogenic H2/O2 Rocket EngineEnhancements to propellants provide an opportunity to either increase performance of an existing vehicle, or reduce the size of a new vehicle. In the late 1980's the National AeroSpace Plane (NASP) reopened the technology chapter on densified propellants, in particular hydrogen. Since that point in time the NASA Lewis Research Center (LERC) in Cleveland, Ohio has been leading the way to provide critical research on the production and transfer of densified propellants. On October 4, 1996 NASA LeRC provided another key demonstration towards the advancement of densified propellants as a viable fuel. Successful ignition of an RL10B-2 engine was achieved with near triple point liquid hydrogen.
Document ID
19970026009
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
McNelis, Nancy B.
(NASA Lewis Research Center Cleveland, OH United States)
Haberbusch, Mark S.
(Ohio Aerospace Inst. Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1997
Subject Category
Propellants And Fuels
Report/Patent Number
E-10758
AIAA Paper 97-2688
NAS 1.15:107470
NASA-TM-107470
Report Number: E-10758
Report Number: AIAA Paper 97-2688
Report Number: NAS 1.15:107470
Report Number: NASA-TM-107470
Meeting Information
Meeting: Joint Propulsion Conference and Exhibit
Location: Seattle, WA
Country: United States
Start Date: July 6, 1997
End Date: July 9, 1997
Sponsors: Society of Automotive Engineers, Inc., American Society of Mechanical Engineers, American Inst. of Aeronautics and Astronautics, American Society for Electrical Engineers
Accession Number
97N25377
Funding Number(s)
PROJECT: RTOP 565-02-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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