Analysis of various transfer missions between parking orbits in cislunar space starting from initial 200 km parking orbit under optimum payload condition discloses interesting correlations between various systems of electric thrustors and missions performed; optimum payload can be calculated from basic formula for electric propulsion systems, which is given; calculated orbits can be correlated to different types of electric propulsion systems, with respect to exhaust velocity and total efficiency. In German with English and French abstracts.
Electric propulsion for cislunar missions
Elektrische Antriebe fuer cislunare Missionen
Astronautica Acta ; 12 , n 1
1966
9 pages
Article (Journal)
English
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