Dynamics of Radially Accelerated Trajectories

• YAMAKAWA Hiroshi

  Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency (JAXA)

抄録

Orbital motion under a continuous outward radial acceleration as a function of the distance from the central body is investigated analytically. The attainable maximum radial distance is given as a function of the radial acceleration, and numerical experiments are carried out showing some periodic orbits under radial acceleration. Three representative cases are treated: constant radial acceleration; radial acceleration proportional to inverse radial distance; and radial acceleration inversely proportional to square of radial distance. This paper focuses on the second case, which has not been reported in the literature. The results are applicable for mini-magnetospheric plasma propulsion.

収録刊行物

• TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

  TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 49 (164), 77-80, 2006

  一般社団法人 日本航空宇宙学会

キーワード

• Orbital Dynamics
• Continuous Thrust
• Radial Acceleration

詳細情報

• CRID: 1390001204080837888
• NII論文ID: 10019370882
• NII書誌ID: AA0086707X
• DOI: 10.2322/tjsass.49.77
• ISSN: 21894205
• ISSN: 05493811
• NDL書誌ID: 8018481
• Web Site: http://id.ndl.go.jp/bib/8018481
• Web Site: https://ndlsearch.ndl.go.jp/books/R000000004-I8018481
• Web Site: https://www.jstage.jst.go.jp/article/tjsass/49/164/49_164_77/_pdf
• 本文言語コード: en
• データソース種別:
  • JaLC
  • NDL
  • Crossref
  • CiNii Articles
• 抄録ライセンスフラグ: 使用不可