@inproceedings{oai:jaxa.repo.nii.ac.jp:00005709,
 author = {福重, 進也 and 赤星, 保浩 and 北澤, 幸人 and 五家, 建夫 and Fukushige, Shinya and Akahoshi, Yasuhiro and Kitazawa, Yukihito and Goka, Tateo},
 book = {宇宙航空研究開発機構特別資料: 第3回宇宙環境シンポジウム講演論文集, JAXA Special Publication: Proceedings of the 3rd Spacecraft Environment Symposium},
 month = {Mar},
 note = {Space agencies of some countries have space debris environment model for design of spacecrafts. These models can estimate debris flux as a function of the size, relative impact velocity, and impact angle in a spacecraft orbit. However, it is known calculation results of models are not always consistent with each other. Therefore, international common implementation process of debris environment model is required. In this paper, as the first step of international standardization of implementation process of debris environment model, we compared estimation results of debris impact flux in low Earth orbit calculated by available three debris environment models, namely NASA's ORDEM2000 (Orbital Debris Engineering Model 2000), ESA's MASTER2001 (Meteoroid and Space debris Terrestrial Environment Reference 2001) and MASTER2005., 資料番号: AA0063585022, レポート番号: JAXA-SP-06-035},
 pages = {117--122},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {デブリ環境モデル(MASTER-2005、2001、ORDEM2000)の比較:宇宙機設計適用プロセスの国際規格化に向けて},
 volume = {JAXA-SP-06-035},
 year = {2007}
}