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Summary Of: Delta-v budget

Encyclodia Page On: Delta-v budget

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astrodynamics | aerospace | delta-v | propulsive | orbital maneuvers | space mission | Hohmann transfer | transfer orbit | slingshot effect | Oberth effect | escape velocity | LEO | atmospheric drag | gravity drag | Re-entry | Station-keeping | geostationary orbit | escape velocity | heat shield | aerobraking | aerocapture | Earth | Low Earth Orbit | Low Earth Orbit | Geostationary Orbit | Lagrangian point 1 | Lagrangian point 2 | Lagrangian point 4/5 | Low Lunar orbit | Moon | Earth | Escape velocity | Earth | Escape velocity | Mars | Transfer Orbit | Mars | Transfer Orbit | Mars | Capture Orbit | Mars | Capture Orbit | Deimos | Transfer Orbit | Deimos | Transfer Orbit | Deimos | Deimos | Transfer Orbit | Phobos | Transfer Orbit | Phobos | Transfer Orbit | Phobos | Mars | Capture Orbit | Mars | Orbit | Mars | Orbit | Mars | Earth | Escape velocity | NEO | Asteroids | Delta-v's in km/s for various orbital maneuvers using conventional rockets. Red arrows show where optional aerobraking can be performed in that particular direction, black numbers give delta-v in km/s that apply in either direction. Lower delta-v transfers than shown can often be achieved, but involve rare transfer windows or take significantly longer, see: fuzzy orbital transfers. Not all possible links are shown. | | fuzzy orbital transfers | Escape orbit | Geosynchronous orbit | Geostationary transfer orbit | Lagrangian point | Low Earth orbit | Low Earth orbit | Kennedy | Bi-elliptic transfer | Gravity assist | Hohmann transfer | The Oberth effect | Tsiolkovsky rocket equation | 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 | Bi-elliptic transfer | Geostationary transfer | Gravity assist | Hohmann transfer | Inclination change | Phasing | Rendezvous | Transposition, docking, and extraction | orbital mechanics | Apsis | Celestial coordinate system | 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 | Celestial mechanics | Orbits | Astrodynamics | Spacecraft propulsion |
This article is licensed under the GNU Free Documentation License. It uses material from the Wikipedia article "Delta-v budget".