@inproceedings{oai:jaxa.repo.nii.ac.jp:00039535,
 author = {宇都宮, 真 and 神谷, 友裕 and 清水, 隆三 and Utsunomiya, Shin and Kamiya, Tomohiro and Shimizu, Ryuzo},
 book = {Proceedings of SPIE},
 month = {Sep},
 note = {SPIE Optics+Photonics 2013 (Aug 25-29, 2013. San Diego Convention Center), San Diego, California, USA., CFRP (Caron fiber reinforced plastics) have superior properties of high specific elasticity and low thermal expansion for satellite telescope structures. However, difficulties to achieve required surface accuracy and to ensure stability in orbit have discouraged CFRP application as main mirrors. We have developed ultra-light weight and high precision CFRP mirrors of sandwich structures composed of CFRP skins and CFRP cores using a replica technique. Shape accuracy of the demonstrated mirrors of 150 mm in diameter was 0.8 μm RMS (Root Mean Square) and surface roughness was 5 nm RMS as fabricated. Further optimization of fabrication process conditions to improve surface accuracy was studied using flat sandwich panels. Then surface accuracy of the flat CFRP sandwich panels of 150 mm square was improved to flatness of 0.2 μm RMS with surface roughness of 6 nm RMS. The surface accuracy vs. size of trial models indicated high possibility of fabrication of over 1m size mirrors with surface accuracy of 1μm. Feasibility of CFRP mirrors for low temperature applications was examined for JASMINE project as an example. Stability of surface accuracy of CFRP mirrors against temperature and moisture was discussed., 資料番号: PA1410032000},
 publisher = {Society of Photo-optical Instrumentation Engineers (SPIE)},
 title = {Development of CFRP mirrors for space telescopes},
 volume = {8837},
 year = {2013}
}