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Cryogenic combustion laboratoryThe objective is to establish a major experimental laboratory for studying fundamental processes such as mixing and combustion under liquid rocket engine conditions. The capability of this laboratory will include operation using a variety of fuel and oxidizer systems including liquid oxygen and liquid hydrocarbons. In addition to providing the proper facilities for supplying and controlling these fuels and oxidizers, a specific effort is being made to provide a state-of-the-art diagnostic capability for combustion measurements. In particular, optical and laser-based techniques are being emphasized for measurements of species, velocities, and spray characteristics.
Document ID
19910018909
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Santoro, R. J.
(Pennsylvania State Univ. University Park, PA, United States)
Kuo, Kenneth K.
(Pennsylvania State Univ. University Park, PA, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1991
Publication Information
Publication: NASA, Washington, Space Transportation Propulsion Technology Symposium. Volume 2: Symposium Proceedings
Subject Category
Spacecraft Propulsion And Power
Accession Number
91N28223
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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