Voyager concept covers orbiting and landing-capsule missions to planets, initially Mars; one possible Voyager concept is considered; spacecraft would consist of bus, propulsion unit, and landing capsule; for orbiting missions propulsion unit would place bus into planetary orbit; Saturn IB/Centaur launch vehicle may be used for Voyager; launch energy requirements and series of Mars missions from 1971 to 1977; characteristics and potential technical problem areas of each module.
Voyager
Astronautics Aeronautics
Astronautics and Aeronautics ; 3 , n 5
1965
6 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Online Contents | 2013
NTRS | 1977
NTRS | 1965
|SLUB | 1987
|Voyager Program: Voyager 2 Encounter at Saturn
NTIS | 1981