Plume mass spectrometry with a hydrazine arcjet thruster

Journal of Spacecraft and Rockets

Volumn 38, Issue 3, 2001, Pages 411-416

  Pollard, James E ^a,d   Masuda, Ideo ^b,e   Gotoh, Yoshifumi ^c,f  

^a AEROSPACE CORPORATION   (United States)

^b Natl Space Dev Agcy Japan   (Japan)

^c MITSUBISHI ELECTRIC CORPORATION   (Japan)

^d Space Materials Laboratory ^*  (United States)

^e Data Relay Test Satellite Project Team   (Japan)

^f Space Systems Department ^*  (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

COMPOSITION EFFECTS; COMPUTER SIMULATION; DISSOCIATION; HYDRAZINE; MASS SPECTROMETRY; MATHEMATICAL MODELS; PRESSURE EFFECTS;

ARCJET THRUSTERS; PLUME MASS SPECTROMETRY;

SPACECRAFT PROPULSION;

EID: 0035332283     PISSN: 00224650     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.3699     Document Type: Article

References (12)

1. Flight qualification of the 1.8 kW MR-509 hydrazine arcjet system
2. Low bus voltage hydrazine arcjet system for geostationary satellites
3. Near-field measurement and modeling results for a flight-type arcjet: NH and H atom
4. A simplified model for prediction of arcjet plumes
5. Arcjet plume studies using molecular beam mass spectrometry
6. Low-power arcjet test facility impacts
7. Supersonic nozzle beams
8. Velocity distributions in molecular beams from nozzle sources
9. Beam experiments at thermal energies
10. Low-energy electron-collision cross section data
11. Studies of low density supersonic jets