Site Navigation
Categories:
Engineering stubs
Celestial mechanics
Orbits
Astrodynamics
Spacecraft propulsion
Orbital maneuvers

Summary Of: Bi-elliptic transfer

The bi-elliptic transfer consists of two half... the bi-elliptic transfer may require a lower amount of total delta... A bi-elliptic transfer from a low circular starting orbit... A bi-elliptic transfer from a low circular starting orbit... A bi-elliptic transfer from a low circular starting orbit... both transfer orbits used in the bi-elliptic transfer constitute exactly one half of an elliptic orbit...

Encyclodia Page On: Bi-elliptic transfer

These Are Links To Other Documents
astronautics | aerospace engineering | orbital maneuver | spacecraft | orbit | delta-v | Hohmann transfer | elliptic orbits | apoapsis | central body | periapsis | semi-major axis | A bi-elliptic transfer from a low circular starting orbit (dark blue), to a higher circular orbit (red). | | vis viva equation | standard gravitational parameter | semi-major axis | magnitude | circular orbit | orbital period | Hohmann transfer orbit | specific orbital energy | Oberth effect | Delta-v budget | The Oberth effect | ISBN 0792369033 | | engineering | stub | help | v | d | Orbits | Box | Capture | Circular | Elliptical | Highly elliptical | Escape | Graveyard | Hyperbolic trajectory | Inclined | Non-inclined | Osculating | Parabolic trajectory | Parking | Synchronous | semi | sub | Geocentric | Geosynchronous | Geostationary | Sun-synchronous | Low Earth | Medium Earth | Molniya | Near-equatorial | Orbit of the Moon | Polar | Tundra | Areosynchronous | Areostationary | Halo | Lissajous | Lunar | Heliocentric | Heliosynchronous | Classical | Inclination | Longitude of the ascending node | Eccentricity | Argument of periapsis | Semi-major axis | Mean anomaly | epoch | True anomaly | Semi-minor axis | Linear eccentricity | Eccentric anomaly | Mean longitude | True longitude | Orbital period | Maneuvers | Geostationary transfer | Gravity assist | Hohmann transfer | Inclination change | Phasing | Rendezvous | Transposition, docking, and extraction | orbital mechanics | Apsis | Celestial coordinate system | Delta-v budget | Epoch | Ephemeris | Equatorial coordinate system | Gravity turn | Ground track | Interplanetary Transport Network | Kepler's laws of planetary motion | Lagrangian point | Low energy transfers | n-body problem | Oberth effect | Orbit equation | Orbital speed | Orbital state vectors | Perturbation | Retrograde and direct motion | Specific orbital energy | Specific relative angular momentum | List of orbits | Categories | Engineering stubs | Celestial mechanics | Orbits | Astrodynamics | Spacecraft propulsion | Orbital maneuvers |
This article is licensed under the GNU Free Documentation License. It uses material from the Wikipedia article "Bi-elliptic transfer".