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Design and Analysis of an APU Monopropellant Gas Generator Rocketdyne Div., North American Rockwell Corporation

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Marcy, R. D., author.
Conference Name:
National Aerospace Engineering and Manufacturing Meeting (1972-10-02 : San Diego, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1972
Summary:
The performance, mechanical integrity, and operational characteristics of a monopropellant thermal gas generator have been predicted using analytical tools developed through the use of digital and analog computer programs. The basis for these analyses are empirical relationships derived from experiments, as well as theoretical relations. A throttleable prototype gas generator has been designed and fabricated to meet the requirements of an APU for use in the Space Shuttle vehicle
Notes:
Vendor supplied data
Publisher Number:
720834
Access Restriction:
Restricted for use by site license

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