Proof-of-concept demonstration of a vaporizing liquid micro-thruster
Author:
Affiliation:
1. JPL, Pasadena, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-3924
Reference5 articles.
1. Thruster options for microspacecraft - A review and evaluation of existing hardware and emerging technologies
2. Propulsion requirements and options for the New Millennium Interferometer (DS-3) Mission
3. The micro-isolation valve - Introduction of concept and preliminary results
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