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Preprints of the Keldysh Institute of Applied Mathematics, 2001, 084
(Mi ipmp1136)
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Ballistic analysis of flight to Mercury with electric propulsion
G. B. Efimov, M. C. Konstantinov, G. G. Fedotov
Abstract:
The ability of flights to Mercury of spacecraft with electrorocket propulsion and solar arrays is proved. The use of “Proton” or “Souz” launchers and the electrorocket propulsion (EP) allow to make a Mercury orbiter. The influence of spacecraft and EP parameters on the payload and trajectory are investigated.
Citation:
G. B. Efimov, M. C. Konstantinov, G. G. Fedotov, “Ballistic analysis of flight to Mercury with electric propulsion”, Keldysh Institute preprints, 2001, 084
Linking options:
https://www.mathnet.ru/eng/ipmp1136 https://www.mathnet.ru/eng/ipmp/y2001/p84
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Statistics & downloads: |
Abstract page: | 94 | Full-text PDF : | 12 |
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