30 cm diameter mercury bombardment low impulse thrustor development for potential space applications, discussing performance and control
Performance and control of a 30-cm-diam, low-impulse, Kaufman thruster
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, ELECTRIC PROPULSION CONFERENCE, 7TH ; 1969 ; WILLIAMSBURG, VA
1970-01-01
Miscellaneous
No indication
English
AIAA | 1969
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