@inproceedings{oai:jaxa.repo.nii.ac.jp:00017504,
 author = {中野, 正勝 and 藤田, 和久 and Viliam, Kmetik and 木皿, 且人 and 新野, 正之 and Nakano, Masakatsu and Fujita, Kazuhisa and Viliam, Kmetik and Kisara, Katsuto and Niino, Masayuki},
 book = {宇宙輸送シンポジウム　平成13年度, Proceedings of Space Transportation Symposium FY2001},
 month = {Apr},
 note = {This paper compares the mission performances of advanced propulsion systems such as electric, solar thermal and laser propulsion systems for GTO-GEO orbit-raising applications. The performance of payload fractions to mission durations was evaluated under the constraints of the Earth shadow and the Van-Allen radiation belts. It was shown that the electric propulsion system can deliver much payload fractions in mission durations over several months, and the solar thermal and laser propulsion systems can deliver much payload fractions in comparison with the chemical propulsion with less radiation damage., 資料番号: AA0033392076},
 pages = {304--307},
 publisher = {宇宙科学研究所, The Institute of Space and Astronautical Science (ISAS)},
 title = {非化学推進による地球周回軌道間移行ミッションの性能評価},
 year = {2002}
}