Systematic comparison of Venus swingby mode with standard mode of Mars round trips
Author:
Affiliation:
1. NASA, OFFICE OF ADVANCED RESEARCH AND TECHNOLOGY, MISSION ANALYSIS DIV., MOFFETT FIELD, CALIF.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1967-27
Reference19 articles.
1. Mars missions," J. Spacecraft and Rockets 1, (Sept.Oct. 1964). 3. Deerwester, J. M. "Initial mas 6 Savings asso
2. ciated with the Venus swingby mode of Mars round trips," A M Paper 65-89 (January 1965). 4. Gillespie, R. W. and Ross, S. E. "The Venus
3. Swingby mission mode and its role in the manned exploration of Mars," AIAA Paper 66-37 (January 1966). > Breakwell, J. V., Gillespie, R. W., and
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1. Use of atmospheric braking during Mars missions;Journal of Spacecraft and Rockets;1990-09
2. Applications of combined electric, high-thrust propulsion systems.;Journal of Spacecraft and Rockets;1968-07
3. Trajectory modes for manned and unmanned missions to Mercury - 1980-2000.;Journal of Spacecraft and Rockets;1967-09
4. Applications of combined high-thrust, low- thrust propulsion systems;3rd Propulsion Joint Specialist Conference;1967-07-17
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