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Minimum impulse technologies for precision attitude control: Minimum Impulse Thruster (MIT) and Hydrazine milliNewton Thruster (HmNT)

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dc.contributor.author Parker, J. M. en_US
dc.date.accessioned 2004-09-16T23:05:08Z
dc.date.available 2004-09-16T23:05:08Z
dc.date.issued 2003-05-06 en_US
dc.identifier.citation DARPA/MTO Workshop: Micro-Thruster Technology for Military Applications en_US
dc.identifier.citation Washington D.C., USA en_US
dc.identifier.clearanceno 03-1066 en_US
dc.identifier.uri http://hdl.handle.net/2014/7308
dc.format.extent 2651708 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other MIT HmNT minimum impulse technologies precision attitude control en_US
dc.title Minimum impulse technologies for precision attitude control: Minimum Impulse Thruster (MIT) and Hydrazine milliNewton Thruster (HmNT) en_US


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