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Jupiter Orbiter Mother/Daughter Spacecraft Concept

Authors :
John H. Duxbury
Source :
Journal of Spacecraft and Rockets. 13:259-260
Publication Year :
1976
Publisher :
American Institute of Aeronautics and Astronautics (AIAA), 1976.

Abstract

The feasibility of a tandem launch of a mother/daughter spacecraft pair with a single launch vehicle for a 1981 Mariner Jupiter Orbiter mission is described. The mother is a close derivative of the three-axis stabilized Mariner Jupiter Saturn 1977 spacecraft with the addition of a Viking-type propulsion module for orbit capture; it concentrates on the planetology and satellite science objectives. The daughter is a small, simple spin-stabilized spacecraft taking advantage of the mother's transit and delivery capabilities; it obtains in-situ measurements of the surrounding planetary environment. A conceptual design of the daughter spacecraft is presented.

Details

ISSN :
15336794 and 00224650
Volume :
13
Database :
OpenAIRE
Journal :
Journal of Spacecraft and Rockets
Accession number :
edsair.doi...........f18e44717a2ddc2db2bda3c11478ac19
Full Text :
https://doi.org/10.2514/3.57085