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Scaling of Performance in Liquid Propellant Rocket Engine Combustion DevicesThis paper discusses scaling of combustion and combustion performance in liquid propellant rocket engine combustion devices. In development of new combustors, comparisons are often made between predicted performance in a new combustor and measured performance in another combustor with different geometric and thermodynamic characteristics. Without careful interpretation of some key features, the comparison can be misinterpreted and erroneous information used in the design of the new device. This paper provides a review of this performance comparison, including a brief review of the initial liquid rocket scaling research conducted during the 1950s and 1960s, a review of the typical performance losses encountered and how they scale, a description of the typical scaling procedures used in development programs today, and finally a review of several historical development programs to see what insight they can bring to the questions at hand.
Document ID
20090001888
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Hulka, James R.
(Jacobs Technologies Engineering Science Contract Group Houston, TX, United States)
Date Acquired
August 24, 2013
Publication Date
July 21, 2008
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: AIAA/ASME/SAE Joint Propulsion Conference
Location: Hartford, CT
Country: United States
Start Date: July 21, 2008
End Date: July 23, 2008
Sponsors: American Society of Mechanical Engineers, Society of Automotive Engineers, Inc., American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNM05AB50C
Distribution Limits
Public
Copyright
Public Use Permitted.
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