Evaluation of High-Power Solar Electric Propulsion Using Advanced Ion, Hall, MPD, and PIT Thrusters for Lunar and Mars Cargo Missions-Reference-Cited by-同舟云学术

Evaluation of High-Power Solar Electric Propulsion Using Advanced Ion, Hall, MPD, and PIT Thrusters for Lunar and Mars Cargo Missions

Published:2006-07-09 Issue: Volume: Page:
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Container-title:42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Frisbee Robert

Publisher

American Institute of Aeronautics and Astronautics

Reference17 articles.

1. Frisbee, R.H.,and Mikellides, I.G. "The Nuclear-Electric Pulsed Inductive Thruster (NuPIT): Mission Analysis for Prometheus,"AIAA Paper AIAA-2005-3892,Presented at the AIAA/ASME/SAE/ASEE 41st Joint Propulsion Conference, Tucson,Arizona,10-13July 2005.

2. Frisbee, R.H.,and Moeller, R.C. "Identification of Mission Sensitivitiesfor High-Power ElectricPropulsion Systems,"AIAA Paper AIAA-2005-3894,Presented at the AIAA/ASME/SAE/ASEE 41st JointPropulsion Conference, Tucson,Arizona,10-13July 2005.

3. Marrese-Reading, C. "The VHITALProgram to Demonstrate the Performance and Lifetimeof a Bismuth-Fueled Very High IspHallThruster,"AIAAPaperAIAA-2005-4564,PresentedattheAIAA/ASME/SAE/ASEE 41stJointPropulsion Conference, Tucson, Arizona, 10-13July 2005.

4. Tikhonov,V.,Semenikhin,S., Alexandrov,V.,Dyakonov,G., and Popov,G. "Research of PlasmaAcceleration Processes in Self-field and Applied MagneticField Thrusters,"IEPCPaper IEPC-93-076,Presented at the23rd International ElectricPropulsion Conference,Seattle WA,1993.

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