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Some three-body numerical solutions to outer planet orbiter missionsusing nuclear-electric propulsion
- Source :
- Astrodynamics Conference.
- Publication Year :
- 1970
- Publisher :
- American Institute of Aeronautics and Astronautics, 1970.
-
Abstract
- Three body numerical solutions to low thrust guidance and navigation for outer planet orbiter with nuclear-electric propulsion
- Subjects :
- Physics
Spacecraft propulsion
business.industry
In-space propulsion technologies
Propulsion
Space exploration
law.invention
Astrobiology
Orbiter
Electrically powered spacecraft propulsion
law
Planet
Astrophysics::Earth and Planetary Astrophysics
Nuclear propulsion
Aerospace engineering
business
Subjects
Details
- Database :
- OpenAIRE
- Journal :
- Astrodynamics Conference
- Accession number :
- edsair.doi...........6997abe4f714b7a61f9256079cf7d49b