方法对比
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| 引力弹弓效应× | 霍曼转移× | |
|---|---|---|
| 领域 | 应用物理学 | 应用物理学 |
| 方法族 | Process / pipeline | Process / pipeline |
| 起源年份≠ | 1961 | 1925 |
| 提出者≠ | Michael Minovitch | Walter Hohmann |
| 类型≠ | Orbital maneuver technique | Trajectory optimization algorithm |
| 开创性文献≠ | Minovitch, M. A. (1961). The determination and characteristics of ballistic interplanetary trajectories under the influence of multiple planetary gravitational fields. Technical Report 32-464, Jet Propulsion Laboratory. link ↗ | Hohmann, W. (1925). Die Erreichbarkeit der Himmelskörper. R. Oldenbourg. link ↗ |
| 别名 | swing-by, gravitational slingshot | Hohmann-Vallado transfer, two-impulse maneuver |
| 相关 | 4 | 4 |
| 摘要≠ | A gravity assist (or swing-by) maneuver uses the gravitational field of a planet or other celestial body to alter a spacecraft's trajectory and velocity without expending fuel. Discovered by Michael Minovitch at JPL in 1961, this technique is crucial for reaching distant planets economically. It works by exploiting the relative motion between the spacecraft, the assisting body, and the Sun. | The Hohmann transfer is a maneuver that transfers a spacecraft between two circular orbits using two impulsive burns (velocity changes). Introduced by German engineer Walter Hohmann in 1925, it is the most fuel-efficient method for coplanar orbital transfers when the transfer time is not severely constrained. The transfer orbit is an ellipse tangent to both the initial and final orbits. |
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