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Minimum impulse technologies for precision attitude control: Minimum Impulse Thruster (MIT) and Hydrazine milliNewton Thruster (HmNT)
Document ID
20060028948
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
hdl:2014/7308
Authors
Parker, J. M.
Date Acquired
August 23, 2013
Publication Date
May 6, 2003
Subject Category
Spacecraft Propulsion And Power
Distribution Limits
Public
Copyright
Other
Keywords
MIT HmNT minimum impulse technologies precision attitude control

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