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Aerobraking

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Aerobraking is a spaceflight maneuver that reduces the high point (apoapsis) of an elliptical orbit by repeatedly flying a spacecraft through the upper atmosphere of a planet at the low point (periapsis) of its orbit, using atmospheric drag to slow the vehicle instead of expending propellant. It has been used to circularize the orbits of several planetary missions, trading a longer approach phase for a large reduction in the fuel mass a spacecraft must carry.

Facts
Concept Domain
Orbital Mechanics 1
Formulated Year
1993 2
Aerobraking was first used operationally during the extended Venusian mission of the Magellan spacecraft in May 1993, and was later used by Mars Global Surveyor, Mars Odyssey and the Mars Reconnaissance Orbiter.
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Sources
1. Wikipedia (space and spaceflight articles)
Wikimedia FoundationAerobraking, lead section
Quote, Aerobraking, lead section
Aerobraking is a spaceflight maneuver that reduces the high point of an elliptical orbit (apoapsis) by flying the vehicle through the atmosphere at the low point of the orbit (periapsis).
1. Wikipedia (space and spaceflight articles)
Wikimedia FoundationAssociated With: Orbital Mechanics
1. Wikipedia (space and spaceflight articles)
Wikimedia FoundationAssociated With: Delta-v
1. Wikipedia (space and spaceflight articles)
Wikimedia FoundationAssociated With: Hohmann Transfer Orbit
2. NASA Solar System Exploration
National Aeronautics and Space AdministrationAerobraking, missions section
Quote, Aerobraking, missions section
In May 1993, aerobraking was used during the extended Venusian mission of the Magellan spacecraft.

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