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Experimental evaluation of high-thrust, throttleable monopropellant hydrazine reactorsHigh thrust throttleable monopropellant hydrazine catalytic reactors for planetary landing vehicles, considering engine designs, dynamic characteristics and response to commanded duty cycles
Document ID
19710050065
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Price, T. W.
Date Acquired
August 6, 2013
Publication Date
June 1, 1971
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 71-705
Report Number: AIAA PAPER 71-705
Meeting Information
Meeting: PROPULSION JOINT SPECIALIST CONFERENCE
Location: SALT LAKE CITY, UT
Country: US
Start Date: June 14, 1971
End Date: June 18, 1971
Sponsors: SOCIETY OF AUTOMOTIVE ENGINEERS, AIAA
Accession Number
71A30762
Distribution Limits
Public
Copyright
Other

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