A Conceptual Design Study of Inexpensive Solar Power Satellite Using Centrifugal Force for Self Deployment

Yasuhiro KURODA; Shinji MATSUMOTO; Kenji NOZAKI; Hisahito TADOKORO; Hiroshi KANAMORI; Kenji TAKAGI

doi:10.11230/jsts.8.2_11

Articles

A Conceptual Design Study of Inexpensive Solar Power Satellite Using Centrifugal Force for Self Deployment

Yasuhiro KURODA, Shinji MATSUMOTO, Kenji NOZAKI, Hisahito TADOKORO, Hiroshi KANAMORI, Kenji TAKAGI

著者情報

キーワード: INEXPENSIVE SOLAR POWER SATELLITE, SELF DEPLOYMENT, CENTRIFUGAL FORCE

ジャーナルフリー

1992 年 8 巻 2 号 p. 2_11-2_15

DOI https://doi.org/10.11230/jsts.8.2_11

詳細

抄録

This paper discusses the concept of constructing inexpensive Solar Power Satellites (SPS) which has the following characteristics; (1) deployable structure, (2) utilization of centrifugal force, (3) no Extra Vehicular Activity (EVA) nor robot, (4) attitude control by natural forces like solar wind and/or magnetic field. Several ideas are evaluated and described.

責任著者(Corresponding author)

J-STAGEへの登録はこちら（無料）