最終更新日:2025/12/07
(astronautics) An elliptical orbit used to transfer a spacecraft between two circular orbits of different altitudes in the same plane, with the periapsis of the orbit being tangent to the smaller circular orbit and its apoapsis being tangent to the larger circular orbit.
音声機能が動作しない場合はこちらをご確認ください
正解を見る
Hohmann transfer
編集履歴(0)