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Trajectory anomalies in interplaneta...

Francisco, Frederico.

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Trajectory anomalies in interplanetary spacecraft = a method for determining accelerations due to thermal emissions and new mission proposals /

Record Type:	Language materials, printed : Monograph/item
Title/Author:	Trajectory anomalies in interplanetary spacecraft/ by Frederico Francisco.
Reminder of title:	a method for determining accelerations due to thermal emissions and new mission proposals /
Author:	Francisco, Frederico.
Published:	Cham :Springer International Publishing : : 2015.,
Description:	xvii, 87 p. :ill., digital ;24 cm.
[NT 15003449]:	Introduction -- The Pioneer Anomaly and Thermal Effects in Spacecraft -- Cassini Gravitational Experiments -- Outer Solar System (OSS) Mission Proposal -- The Flyby Anomaly and Options for Its Study -- Conclusions and Outlook.
Contained By:	Springer eBooks
Subject:	Space trajectories. -
Online resource:	http://dx.doi.org/10.1007/978-3-319-18980-2
ISBN:	9783319189802 (electronic bk.)

Trajectory anomalies in interplanetary spacecraft = a method for determining accelerations due to thermal emissions and new mission proposals /
Francisco, Frederico.

Trajectory anomalies in interplanetary spacecrafta method for determining accelerations due to thermal emissions and new mission proposals /[electronic resource] :by Frederico Francisco. - Cham :Springer International Publishing :2015. - xvii, 87 p. :ill., digital ;24 cm. - Springer theses,2190-5053. - Springer theses..

Introduction -- The Pioneer Anomaly and Thermal Effects in Spacecraft -- Cassini Gravitational Experiments -- Outer Solar System (OSS) Mission Proposal -- The Flyby Anomaly and Options for Its Study -- Conclusions and Outlook.

This thesis presents fundamental work that explains two mysteries concerning the trajectory of interplanetary spacecraft. For the first problem, the so-called Pioneer anomaly, a wholly new and innovative method was developed for computing all contributions to the acceleration due to onboard thermal sources. Through a careful analysis of all parts of the spacecraft Pioneer 10 and 11, the application of this methodology has yielded the observed anomalous acceleration. This marks a major achievement, given that this problem remained unsolved for more than a decade. For the second anomaly, the flyby anomaly, a tiny glitch in the velocity of spacecraft that perform gravity assisting maneuvers on Earth, no definitive answer is put forward; however a quite promising strategy for examining the problem is provided and a new mission is proposed. The proposal largely consists in using the Galileo Navigational Satellite System to track approaching spacecraft, and in considering a small test body that approaches Earth from a highly elliptic trajectory.

ISBN: 9783319189802 (electronic bk.)

Standard No.: 10.1007/978-3-319-18980-2doiSubjects--Topical Terms:

1641540
Space trajectories.

LC Class. No.: TL1075

Dewey Class. No.: 629.411

Trajectory anomalies in interplanetary spacecraft = a method for determining accelerations due to thermal emissions and new mission proposals /
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505 0 $a Introduction -- The Pioneer Anomaly and Thermal Effects in Spacecraft -- Cassini Gravitational Experiments -- Outer Solar System (OSS) Mission Proposal -- The Flyby Anomaly and Options for Its Study -- Conclusions and Outlook.
520 $a This thesis presents fundamental work that explains two mysteries concerning the trajectory of interplanetary spacecraft. For the first problem, the so-called Pioneer anomaly, a wholly new and innovative method was developed for computing all contributions to the acceleration due to onboard thermal sources. Through a careful analysis of all parts of the spacecraft Pioneer 10 and 11, the application of this methodology has yielded the observed anomalous acceleration. This marks a major achievement, given that this problem remained unsolved for more than a decade. For the second anomaly, the flyby anomaly, a tiny glitch in the velocity of spacecraft that perform gravity assisting maneuvers on Earth, no definitive answer is put forward; however a quite promising strategy for examining the problem is provided and a new mission is proposed. The proposal largely consists in using the Galileo Navigational Satellite System to track approaching spacecraft, and in considering a small test body that approaches Earth from a highly elliptic trajectory.
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