A Comparison of Low Thrust Cryogenic Propulsion and Solar Thermal Propulsion

Author:

Valentian Dominique,Amari Moussa,Fratacci Georges,Melchior Antoine

Publisher

American Institute of Aeronautics and Astronautics

Reference4 articles.

1. E.C Cady: Solar thermal upper stage technology demonstrator, liquid hydrogen storage and feed systemtest program. STAIF 1997 conf. 970115 American Institute of Physics, Albuquerque February1997

2. Robert Zubrin et Al: Exploration missions with asolarbimodal system. STAIF 1997 conf. 970115 American Institute of Physics, Albuquerque February1997

3. ChristopheKoppel Benefits of the plasmic propulsion for performing the orbit transfer and the station keeping .19thICSSC. AIAA / CNES / ESA / SUP AERO conference17-20April 2001.Toulouse

4. Zero Boil Off Cryogen Storage For Future Launchers Salerno L.J., Valentian D., Plachta D. W., Kittel P., Hastings L.J., S 9.5 (89) Third European conference on Launcher Technology, 11-14Dec. 2001, Strasbourg,France

Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Applications of Low Cost Cryogenic Propulsion to New Launchers and Planetary Missions Concepts;41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2005-07-10

2. A Low Cost Cryogenic Propulsion Module for Commercial and Planetary Missions;39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2003-06-26

3. Single-Crystal Molybdenum Solar Thermal Propulsion Thruster;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2003

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