@inproceedings{oai:jaxa.repo.nii.ac.jp:00005225,
 author = {荒川, 陽司 and Arakawa, Yoji},
 book = {宇宙航空研究開発機構特別資料, JAXA Special Publication: Proceedings of International Symposium on "SM/MPAC & SEED Experiment"},
 month = {Mar},
 note = {International Symposium on "SM/MPAC & SEED Experiment" (International Congress Center EPOCHAL TSUKUBA, 10-11 March 2008), Polymer matrix composites such as carbon fiber reinforced plastic (CFRP) are lightweight materials which have good mechanical properties and are applied widely as basic structural materials for spacecraft, especially reusable launch vehicle. However the degradation data of the CFRP after exposed in space environment for long period was not obtained in ground experiment. Therefore understanding the process of degradation for CFRP is very important to maintain structural reliability. In this study we evaluate the two heat resistant CFRP which are candidates for the reusable launch vehicle., Physical characteristics: Original contains color illustrations, 資料番号: AA0064307009, レポート番号: JAXA-SP-08-015E},
 pages = {67--71},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {Influence on polymer matrix composite exposed to space environment},
 volume = {JAXA-SP-08-015E},
 year = {2009}
}