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Feasibility Investigation for Performing Fireball Temperature TestsNASA Johnson Space Center White Sands Test Facility (WSTF) was requested by the Launch Abort Subpanel and the Power Systems Subpanel of the Interagency Nuclear Safety Review Panel to investigate the feasibility of using spectroscopic techniques to measure propellant fireball gas temperatures. This report outlines the modeling and experimental approaches and results of this investigation. Descriptions of the theoretical particle temperature and mass effusion models are presented along with the results of the survivability of small plutonium dioxide (less than or equal to 1000 microns diameter) particles entrained in various propellant fireball scenarios. The experimental test systems used to measure the hydroxide radical, water, and particle graybody spectral emissions and absorptions are discussed. Spectral results along with temperatures extracted by analyzing the spectral features are presented for the flames investigated in the laboratory environment. Methods of implementing spectroscopic measurements for future testing using the WSTF Large-scale Hydrogen/Oxygen Explosion Facility are discussed, and the accuracy expected for these measurements is estimated from laboratory measurements.
Document ID
19980219369
Acquisition Source
White Sands Test Facility
Document Type
Other
Authors
Tapphorn, Ralph M.
(Allied-Signal Technical Services Corp. Las Cruces, NM United States)
Kurtz, Joe
(Allied-Signal Technical Services Corp. Las Cruces, NM United States)
Date Acquired
September 6, 2013
Publication Date
March 11, 1997
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
TR-757-001
Report Number: TR-757-001
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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