Due to their simplicity, low-thrust cold-gas propulsion systems have the potential to provide orbital maneuvering capability for small, micro- and even nano-satellites. Each specific mission where cold gas thrusters will be used places a unique set of requirements on the system. For example, micro- spacecraft with masses of 1 - 50 kg, will require thrust levels for typical orbital maintenance maneuvers of 0.1 - 1OmN.
Numerical Study of Cold Gas Micronozzle Flows
1999
15 pages
Report
Keine Angabe
Englisch
Numerical Study of Cold Gas Micronozzle Flows
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