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Design and Activation of a LOX/GH Chemical Steam GeneratorThe purpose of this paper is to give a detailed description of the design and activation of the LOX/GH fueled chemical steam generator installed in Cell 2 of the E3 test facility at Stennis Space Center, MS (SSC). The steam generator uses a liquid oxygen oxidizer with gaseous hydrogen fuel. The combustion products are then quenched with water to create steam at pressures from 150 to 450 psig at temperatures from 350 to 750 deg F (from saturation to piping temperature limits).
Document ID
20100021225
Acquisition Source
Stennis Space Center
Document Type
Conference Paper
Authors
Saunders, G. P. (NASA Stennis Space Center Stennis Space Center, MS, United States)
Mulkey, C. A. (NASA Stennis Space Center Stennis Space Center, MS, United States)
Taylor, S. A. (NASA Stennis Space Center Stennis Space Center, MS, United States)
Date Acquired
August 24, 2013
Publication Date
August 3, 2009
Subject Category
Propellants And Fuels
Report/Patent Number
SSTI-8080-0035
Meeting Information
Meeting: 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Location: Denver, CO
Country: United States
Start Date: August 3, 2009
End Date: August 5, 2009
Sponsors: American Society for Engineering Education, American Inst. of Aeronautics and Astronautics, American Society for Engineering Education, Society of Automotive Engineers, Inc.
Funding Number(s)
TASK: NNS04AB67T
Distribution Limits
Public
Copyright
Public Use Permitted.

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