宇宙用大型反射鏡のモジュール熱変形評価

概要

論文の詳細を見る
Thermal distortion of a large deployable reflector, for use on board a satellite, was evaluated using an artificial environmental chamber. The large deployable reflector, which is 15 m in diameters, was developed based on a modular concept in which the structure consists of several basic modules about 5 m in diameter. Each basic module consists of a mesh surface, a cable network, and a truss structure. The mesh used for the reflector surface reduces the weight, and the cable network is formed so that the mesh surface is parabolic in shape. The truss structure maintains the length of cable and the form of the mesh surface.
一般社団法人日本機械学会の論文
2000-06-25