Solar electric propulsion leverage: Electric delta-VEGA (EDVEGA) scheme and its application

研究成果: Conference article査読

13 被引用数 (Scopus)

抄録

The extended strategy EDVEGA (Electric Delta-VEGA) is presented. What is stressed is the use of 1.4-year singular trajectory that preserves the encounter period with the Earth regardless of how much delta-V excess is garnered and embedded. The biggest advantage is, first of all, that the electric propulsion is performed efficiently at 1 AU distance. The other advantages are that the Earth launch C3 can be reduced to zero and the declination angle constraint is avoided. Some analytic efficiency evaluation method and numerical examination are carried out. The strategy can be widely applied for the outer space explorations.

本文言語English
ページ(範囲)1577-1586
ページ数10
ジャーナルAdvances in the Astronautical Sciences
108 II
出版ステータスPublished - 2001
外部発表はい
イベントProceedings of the AAS/AIAA Space Flight Mechanics Meeting - Santa Barbara, CA, United States
継続期間: 2001 2 112001 2 15

ASJC Scopus subject areas

  • 航空宇宙工学
  • 宇宙惑星科学

フィンガープリント

「Solar electric propulsion leverage: Electric delta-VEGA (EDVEGA) scheme and its application」の研究トピックを掘り下げます。これらがまとまってユニークなフィンガープリントを構成します。

引用スタイル