Computer Science – Performance
Scientific paper
Oct 2004
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2004esasp.555e..67m&link_type=abstract
Proceedings of the 4th International Spacecraft Propulsion Conference (ESA SP-555). 2-9 June, 2004, Chia Laguna (Cagliari), Sard
Computer Science
Performance
Scientific paper
Pyrotechnic actuated valves are currently used extensively in satellite chemical propulsion systems. These valves serve as isolation valves. They are single- use, of very high reliability, and used to initiate a propulsion system at the start of its propulsion mission or to "safe" it at the end of its mission life. A new type of valve is currently in its initial stages of development which aims to replace the pyro with a Shape Memory Alloy (SMA) actuator. This valve would give the same isolation performance, would work at high temperature up to 100°C, could be much slower limiting mechanical shocks, and be interchangeable with pyro-valves making substitution simple. This paper outlines the scope of this work.
Lanfranconi R.
Mignon A.
Murray James
Promper Christophe
Stalmans R.
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