@inproceedings{oai:jaxa.repo.nii.ac.jp:00038078,
 author = {青木, 圭一 and 矢部, 孝 and 中川, 順達 and 尾形, 陽一 and Aoki, Keiichi and Yabe, Takashi and Nakagawa, Masamichi and Ogata, Yoichi},
 book = {航空宇宙技術研究所特別資料: 航空宇宙数値シミュレーション技術シンポジウム2001論文集, Special Publication of National Aerospace Laboratory: Proceedings of Aerospace Numerical Simulation Symposium 2001},
 month = {Jan},
 note = {In this paper, the numerical calculations of laser propulsion for space vehicle are discussed. For calculating the behavior of ablation, it is necessary to do with the solid, the liquid and the gas at the same time. This process was calculated with the hydrocode based on a highly-accurate scheme CIP-CUP (Cubic-Interpolated Pseudoparticle Combined Unified Procedure) method. With this scheme, the efficiency by C(sub m) (the momentum coupling coefficient) is evaluated for the cases of single pulse and some target shapes. In order to confirm the result, experiments were performed with a pendulum and a semi-conductor load-cell., 資料番号: AA0032819042, レポート番号: NAL SP-53},
 pages = {245--250},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {レーザーアブレーションによる飛翔体推進の効率化},
 volume = {53},
 year = {2002}
}