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
01.01.1970
Sonstige
Keine Angabe
Englisch
AIAA | 1969
|