Solar Thermal Propulsion System for Microsatellites Orbit Transferring-Reference-Cited by-同舟云学术

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Solar Thermal Propulsion System for Microsatellites Orbit Transferring

Published:2004-06-26 Issue: Volume: Page:
ISSN:
Container-title:40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
language:
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Author:

Sahara Hironori¹,Shimizu Morio²

Affiliation:

1. University of Tokyo

2. Japan Aerospace Exploration Agency

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-3764

Reference13 articles.

1. 2Kudija,C."TheIntegratedSolarUpperStage(ISUS)EngineGroundDemonstration(EGD),"AIAAPaper,AIAA96-3043, 1996.

2. 3Partch,R."SolarOrbitTransferVehicleSpaceExperimentConceptualDesign,"AIAAPaper,AIAA-99-2476,June1999.

3. 5Shimizu,M.etal."LargeSolarThermalThrusterMadeofSingleCrystalMolybdenum,"IAF-00-S.6.01,Oct.2000.

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1. Design and characterisation of a bi-modal solar thermal propulsion and power system for small satellites;Applied Thermal Engineering;2021-05

2. Cost analysis of solar thermal propulsion systems for microsatellite applications;Acta Astronautica;2019-02

3. Molten Boron Phase-Change Thermal Energy Storage to Augment Solar Thermal Propulsion Systems;47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2011-07-31

4. A Review of High Thrust, High Delta-V Options for Microsatellite Missions;45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2009-08-02

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