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ELECTRIC PROPULSION SYSTEMS
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Language:
English
Abstract
THE NUCLEAR turboelectric ion propulsion system operates as follows:
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1.
A nuclear reactor supplies thermal energy to a vapor boiler.
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2.
The vapor drives a turbine, which operates an electric generator.
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3.
The electric power is used to ionize and accelerate the propellant — a liquid alkali metal — which produces the thrust.
Electric propulsion systems can be used in a wide variety of space missions, including satellite sustainers, lunar cargo transport, and interplanetary missions.*
Authors
Citation
Kovacik, V. and Ross, D., "ELECTRIC PROPULSION SYSTEMS," SAE Technical Paper 600043, 1960, https://doi.org/10.4271/600043.Also In
References
- “Performance of Nuclear Electric Propulsion Systems,” Kovacik V. P. Ross. D. P. Paper presented at IAS Annual Meeting New York January 1959
- “Comparative Performance of Ballistic and Low-Thrust Vehicles for Flight to Mars,” Irving J. H. Blum. E. K. Paper presented at Second Annual AFOSR Astronautics Symposium Denver April 1958
- “Estimating Missile Proportions,” Dobrin. Saxe Dr. Aircraft and Missiles Manufacturing Vol. 1 April 1958