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- Bi-elliptic_transfer abstract "In astronautics and aerospace engineering, the bi-elliptic transfer is an orbital maneuver that moves a spacecraft from one orbit to another and sometimes requires 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 away from the central body. At this point a second burn sends the spacecraft into the second elliptical orbit with periapsis at the radius of the final desired orbit, where a third burn is performed, injecting the spacecraft into the desired orbit.[citation needed]While they require one more engine burn than a Hohmann transfer and generally requires a greater travel time, some bi-elliptic transfers require a lower amount of total delta-v than a Hohmann transfer when the ratio of final to initial semi-major axis is 11.94 or greater, depending on the intermediate semi-major axis chosen.Ary Sternfeld in 1934 first[citation needed] published the idea of the bi-elliptical transfer trajectory.".
- Bi-elliptic_transfer thumbnail Bi-elliptic_transfer.svg?width=300.
- Bi-elliptic_transfer wikiPageID "3383505".
- Bi-elliptic_transfer wikiPageRevisionID "603518538".
- Bi-elliptic_transfer hasPhotoCollection Bi-elliptic_transfer.
- Bi-elliptic_transfer subject Category:Astrodynamics.
- Bi-elliptic_transfer subject Category:Orbital_maneuvers.
- Bi-elliptic_transfer subject Category:Spacecraft_propulsion.
- Bi-elliptic_transfer type Abstraction100002137.
- Bi-elliptic_transfer type Act100030358.
- Bi-elliptic_transfer type Activity100407535.
- Bi-elliptic_transfer type Event100029378.
- Bi-elliptic_transfer type Maneuver100959992.
- Bi-elliptic_transfer type Operation100955060.
- Bi-elliptic_transfer type OrbitalManeuvers.
- Bi-elliptic_transfer type PsychologicalFeature100023100.
- Bi-elliptic_transfer type YagoPermanentlyLocatedEntity.
- Bi-elliptic_transfer comment "In astronautics and aerospace engineering, the bi-elliptic transfer is an orbital maneuver that moves a spacecraft from one orbit to another and sometimes requires 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 away from the central body.".
- Bi-elliptic_transfer label "Bi-elliptic transfer".
- Bi-elliptic_transfer label "Transferência bielíptica".
- Bi-elliptic_transfer label "Trasferimento alla Sternfeld".
- Bi-elliptic_transfer sameAs Transfer_bi-eliptik.
- Bi-elliptic_transfer sameAs Trasferimento_alla_Sternfeld.
- Bi-elliptic_transfer sameAs Transferência_bielíptica.
- Bi-elliptic_transfer sameAs m.098rc6.
- Bi-elliptic_transfer sameAs Q3997712.
- Bi-elliptic_transfer sameAs Q3997712.
- Bi-elliptic_transfer sameAs Bi-elliptic_transfer.
- Bi-elliptic_transfer wasDerivedFrom Bi-elliptic_transfer?oldid=603518538.
- Bi-elliptic_transfer depiction Bi-elliptic_transfer.svg.
- Bi-elliptic_transfer isPrimaryTopicOf Bi-elliptic_transfer.