Solution to problem of transferring rocket from circular orbit about one planet into another about second planet with minimum expenditure of fuel; planetary orbits assumed to be coplanar and longitudes of planets in their orbits at instants of departure and arrival of rocket, supposed to be specified; case of transfer between Earth and Mars taken as numerical example.
Transfer between circular orbits
Jet Propulsion
Jet Propulsion ; 26 , n 7, Part 1
1956
4 pages
Article (Journal)
English
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