Fundamentals of electric propulsion; description and characteristics of three types of thrust devices -- electrostatic accelerators, electromagnetic accelerators, and thermal arc jets; possible missions listed which could be applicable for electric propulsion; power requirements presented in parametric form for specific missions of low-altitude sustainer and orbit transfers; off-optimum operations are considered in case of 200 to 22,300 mi orbit transfer.
Electric propulsion and power requirements for space vehicles
SAE -- Paper
SAE Meeting ; 1960 Electric propulsion
1960
14 pages
Aufsatz (Konferenz)
Englisch
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ELECTRIC PROPULSION AND POWER REQUIREMENTS FOR SPACE VEHICLES
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