Development and demonstration of a 1.8 kW hydrazine arcjet thruster
Author:
Affiliation:
1. Rocket Research Co., Redmond, WA
2. General Electric Co., Astro-Space Div., Princeton, NJ
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1990-2547
Reference5 articles.
1. Design, testing, and integration of a flight-ready hydrazine arcjet system
2. Life demonstration test of an uprated Augmented Catalytic Thruster
3. Low power arcjet life issues
4. Performance characterization of a low power hydrazine arcjet
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