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Jupiter Orbiter Mother/Daughter Spacecraft Concept
- 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.
- Subjects :
- Physics
Spacecraft
Unmanned spacecraft
business.industry
Aerospace Engineering
Spacecraft design
Orbital station-keeping
law.invention
Astrobiology
Quantitative Biology::Subcellular Processes
Jupiter
Service module
Orbiter
Space and Planetary Science
law
Physics::Space Physics
Astrophysics::Earth and Planetary Astrophysics
Orbital maneuver
business
Subjects
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