Near-field measurement and modeling results for flight-type arcjet: Hydrogen atom

Journal of Spacecraft and Rockets

Volumn 38, Issue 3, 2001, Pages 417-425

  Crofton, Mark W ^a,e   Moore, Teresa A ^a,e   Boyd, Iain D ^b,f   Masuda, Ideo ^c,g   Gotoh, Yoshifumi ^d,h  

^a AEROSPACE CORPORATION   (United States)

^b UNIVERSITY OF MICHIGAN   (United States)

^c Natl Space Dev Agcy Japan   (Japan)

^d MITSUBISHI ELECTRIC CORPORATION   (Japan)

^e Propulsion Science and Experimental Mechanics Department   (United States)

^f Department of Aerospace Engineering ^*  (United States)

^g Data Relay Test Satellite Project Team   (Japan)

^h Space Systems Department ^*  (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; DECOMPOSITION; FLUORESCENCE; HYDRAZINE; HYDROGEN; LASER APPLICATIONS; MATHEMATICAL MODELS; MONTE CARLO METHODS;

ARCJETS;

SPACECRAFT PROPULSION;

EID: 0035332208     PISSN: 00224650     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.3700     Document Type: Article

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6. Quantitative two-photon laser-induced fluorescence of hydrogen atoms in a 1 kW arcjet thruster
7. Stark broadening corrections to laser-induced fluorescence temperature measurements in a hydrogen arcjet plume
8. Near-field measurement and modeling results for flight-type arcjet: NH molecule
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11. + state
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15. Extensive validation of a Monte Carlo model for hydrogen arcjet flowfields
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18. Advances in plasma broadening of atomic hydrogen
19. Hydrogen stark-broadening tables
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22. 2 discharges
23. Two-photon-excited stimulated emission from atomic hydrogen in flames
24. Angular momentum state mixing and quenching of n = 3 atomic hydrogen fluorescence
25. 2 molecule
26. Plume mass spectrometry with a hydrazine arcjet thruster