Motion of planets in relation to each other, and conditions for attaining orbits of artificial satellites and trajectories of space probes are considered; 3- and n-body problems and their periodic solutions are briefly discussed; basic equations are given for rocket propulsion; first determination of trajectory based on vector of trajectorial velocity, importance of trajectory corrections, difficulties of trajectory to moon, and requirements for traveling to nearby planets are discussed. (See also v 106 n 13 May (I) 1964 p 545-51)
Physical and astronomical principles of satellite and space flight
Physikalische und astronomische Grundlagen des Satelliten- und des Welgraumflugs
VDI -- Zeitschrift ; 106 , n 15
1964
6 pages
Article (Journal)
German
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