Near-earth missions, such as placing stationary satellite in orbit, call for specific impulse ranges natural to plasmajet systems; flight parameters for round trip to lunar orbit; possible methods of achieving specific impulses for missions contemplated within gravitational field of earth; development of thrust devices, divided into nonconducting gas, electrostatic acceleration devices, (ion rockets), and neutral plasma devices.
Plasma propulsion of spacecraft
Astronautics
Astronautics ; 4 , n 10
1959
3 pages
Aufsatz (Zeitschrift)
Englisch
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