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单词 Hohmann trajectory
释义

Hohmann trajectory

中文百科

霍曼转移轨道 Hohmann transfer orbit

(重定向自Hohmann trajectory)
霍曼转移轨道为图中编号2的半椭圆轨道
A costly naive non-Hohmann transfer from a low circular orbit to a higher circular orbit using high thrust
die für den Hohmann-Transfer nötige Geschwindigkeitsänderung in Abhängigkeit vom Geschwindigkeitsverhältnis von Ausgangs- und Zielorbit

在太空动力学,霍曼转移轨道(或译为郝曼转移轨道Hohmann transfer orbit)是一种变换太空船轨道的方法,途中只需两次引擎推进,相对地节省燃料。此种轨道操纵名称来自德国物理学家瓦尔特·霍曼,他于1925年出版了相关著作。

英语百科

Hohmann transfer orbit 霍曼转移轨道

(重定向自Hohmann trajectory)
Hohmann transfer orbit, labelled 2, from a low orbit (1) to a higher orbit (3).
A costly naive non-Hohmann transfer from a low circular orbit to a higher circular orbit using high thrust

In orbital mechanics, the Hohmann transfer orbit /ˈh.mʌn/ is an elliptical orbit used to transfer between two circular orbits of different radii in the same plane.

The orbital maneuver to perform the Hohmann transfer uses two engine impulses, one to move a spacecraft onto the transfer orbit and a second to move off it. This maneuver was named after Walter Hohmann, the German scientist who published a description of it in his 1925 book Die Erreichbarkeit der Himmelskörper ("The Accessibility of Celestial Bodies") Hohmann was influenced in part by the German science fiction author Kurd Lasswitz and his 1897 book Two Planets.

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