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Measuring the Thermal Accommodation Coefficient while Aerobraking Magellan

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dc.contributor.author Lyons, Daniel T. en_US
dc.contributor.author Buescher, Joe en_US
dc.contributor.author Esterl, Greg en_US
dc.contributor.author Neuman, James en_US
dc.date.accessioned 2004-10-05T05:18:56Z
dc.date.available 2004-10-05T05:18:56Z
dc.date.issued 1994-07-25 en_US
dc.identifier.citation Oxford, England en_US
dc.identifier.clearanceno 94-1094 en_US
dc.identifier.uri http://hdl.handle.net/2014/33160
dc.description.abstract The Magellan spacecraft was inserted into an elliptical orbit around the planet Venus on August 10, 1990. A small aerodynamic force was applied later to the spacecraft for 730 consecutive orbits to lower the apoapsis of the orbit from 8500 km to 541 km. Atmospheric drag removed a maximum of 2 m/sec per orbit from the velocity at periapsis for a total delta-V of 1200 m/sec. This paper will discuss the thermal accommodation coefficient which was inferred from one of the four solar panel temperature measurements from the aerobraking pass through the atmosphere. en_US
dc.format.extent 255072 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other aerobraking orbits Venus Magellan aerodynamic forces delta-V temperature measurements thermal accomodation coefficient en_US
dc.title Measuring the Thermal Accommodation Coefficient while Aerobraking Magellan en_US


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