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Bi-elliptic transfer - Wikipedia, the free encyclopedia

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Clipped on: 2014-11-08

Bi-elliptic transfer

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In astronautics and aerospace engineering, the bi-elliptic transfer is an orbital maneuver that moves a spacecraft from one orbit to another and may, in certain situations, require less delta-v than a Hohmann transfer maneuver.

The bi-elliptic transfer consists of two half elliptic orbits. From the initial orbit, a first burn expends delta-v to boost the spacecraft into the first transfer orbit with an apoapsis at some point Image (Asset 1/28) alt=