NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Radiative properties of molecular nitrogen ions produced by helium Penning ionization and argon effectsThe development of hypersonic aerospace vehicles requires a better understanding on the thermal and chemical nonequilibrium kinetics of participating species in shock layers. The computational fluid dynamic (CFD) codes developed for such flowfields overestimate the radiation in the spectral region of 300 - 600 nm. A speculation for this overestimation is that inclusion of Ar, CO2, and H2O at the upper atmosphere flight region makes a significant impact on radiative kinetics of molecular nitrogen ions. To define the effects of minority species on the radiative kinetics of N2(+), an experimental setup was made by using the helium Penning ionization. The vibrational and rotational temperature were measured by mapping the vibrational and rotational distributions of N2(+) emission with high spectroscopic resolution and absolute intensity measurements. Measured vibrational temperatures were in the range from 18,000 to 36,000 K, and rotational temperatures were in the range from 300 to 370 K. The irradiance of 391.44 nm line and rotational and vibrational temperatures were analyzed to define argon and CO2 effects on the N2(+) emission. When Ar or CO2 is injected with N2, the rotational temperature did not change. The irradiances were reduced by 34 percent and 78 percent for the 50 percent of mixture of Ar and CO2, respectively. The vibrational temperatures were increased by 24.1 percent and 82.9 percent for the 50 percent of mixture of Ar and CO2, respectively. It appears that there are no significant effects from small concentrations of Ar and CO2 at the upper atmosphere flight region.
Document ID
19940020014
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Miller, George, III
(Norfolk State Univ. VA, United States)
Song, Kyo-Dong
(Norfolk State Univ. VA, United States)
Date Acquired
September 6, 2013
Publication Date
February 4, 1994
Subject Category
Atomic And Molecular Physics
Report/Patent Number
NAS 1.26:195126
NASA-CR-195126
Report Number: NAS 1.26:195126
Report Number: NASA-CR-195126
Accession Number
94N24487
Funding Number(s)
CONTRACT_GRANT: NAG1-1513
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available