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Boost-phase discrimination researchThe final report describes the combined work of the Computational Chemistry and Aerothermodynamics branches within the Thermosciences Division at NASA Ames Research Center directed at understanding the signatures of shock-heated air. Considerable progress was made in determining accurate transition probabilities for the important band systems of NO that account for much of the emission in the ultraviolet region. Research carried out under this project showed that in order to reproduce the observed radiation from the bow shock region of missiles in their boost phase it is necessary to include the Burnett terms in the constituent equation, account for the non-Boltzmann energy distribution, correctly model the NO formation and rotational excitation process, and use accurate transition probabilities for the NO band systems. This work resulted in significant improvements in the computer code NEQAIR that models both the radiation and fluid dynamics in the shock region.
Document ID
19940015345
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Langhoff, Stephen R.
(NASA Ames Research Center Moffett Field, CA, United States)
Feiereisen, William J.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 6, 2013
Publication Date
July 7, 1993
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-TM-109347
NAS 1.15:109347
AD-A270939
ARO-27469.1-EG-SDI
Report Number: NASA-TM-109347
Report Number: NAS 1.15:109347
Report Number: AD-A270939
Report Number: ARO-27469.1-EG-SDI
Accession Number
94N19818
Funding Number(s)
CONTRACT_GRANT: MIPR-135-92
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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