NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Scaling of Performance in Liquid Propellant Rocket Engine CombustorsThis 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
20070036780
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Hulka, James R.
(Jacobs Engineering Group, Inc. Huntsville, AL, United States)
Date Acquired
August 24, 2013
Publication Date
March 7, 2007
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: 20th Memorial meeting of the Northern Section of the Japan Society for Aeronautical and Space Sciences (JSASS)
Location: Sendai
Country: Japan
Start Date: March 7, 2007
End Date: March 9, 2007
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available