NASA NTRS · 20060028948
Minimum impulse technologies for precision attitude control: Minimum Impulse Thruster (MIT) and Hydrazine milliNewton Thruster (HmNT)
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Parker, J. M.. 2003-05-06. Minimum impulse technologies for precision attitude control: Minimum Impulse Thruster (MIT) and Hydrazine milliNewton Thruster (HmNT). https://ntrs.nasa.gov/citations/20060028948
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