Mission Capability Gains from Multi-Mode Propulsion Thrust Profile Variations for a Plane Change Maneuver-Reference-Cited by-同舟云学术

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Mission Capability Gains from Multi-Mode Propulsion Thrust Profile Variations for a Plane Change Maneuver

Published:2011-06-14 Issue: Volume: Page:
ISSN:
Container-title:AIAA Modeling and Simulation Technologies Conference
language:
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Author:

Rexius Tiffany¹,Holmes Michael¹

Affiliation:

1. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-6431

Reference7 articles.

1. Spacecraft optimization with combined chemical-electric propulsion

2. 3Bate,Roger,Mueller,Donald,&White,Jerry.(1971).FundamentalsofAstrodynamics.DoverPubns.

3. 4Petter,M.,Heilman,S."MultipleModePropulsionsystemforSpacecraftOrbitTransfer,Maneuvering,andAttitude Control,"BAA-06-02-PKTB. (24April 2006).

4. 5Humble,Ronald,Henry,Gary,&Larson,Wiley.(1995).Spacepropulsionanalysisanddesign.LearningSolutions.

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1. Review of Chemical-Electric Multimode Space Propulsion;AIAA Propulsion and Energy 2019 Forum;2019-08-16

2. Characterization of a Novel Ionic Liquid Monopropellant for Multi-Mode Propulsion;53rd AIAA/SAE/ASEE Joint Propulsion Conference;2017-07-07

3. Assessment of Multimode Spacecraft Micropropulsion Systems;Journal of Spacecraft and Rockets;2017-05

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