國立虎尾科技大學 |

Trajectory Anomalies in Interplanetary Spacecraft = A Method for Determining Accelerations Due to Thermal Emissions and New Mission Proposals /

紀錄類型:	書目-語言資料,印刷品 : Monograph/item
正題名/作者:	Trajectory Anomalies in Interplanetary Spacecraft/ by Frederico Francisco.
其他題名:	A Method for Determining Accelerations Due to Thermal Emissions and New Mission Proposals /
作者:	Francisco, Frederico.
面頁冊數:	XVII, 87 p. 27 illus., 3 illus. in color.online resource. :
Contained By:	Springer Nature eBook
標題:	Astronautics. -
電子資源:	https://doi.org/10.1007/978-3-319-18980-2
ISBN:	9783319189802

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. - 1st ed. 2015. - XVII, 87 p. 27 illus., 3 illus. in color.online resource. - Springer Theses, Recognizing Outstanding Ph.D. Research,2190-5053. - Springer Theses, Recognizing Outstanding Ph.D. Research,.

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

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

646219
Astronautics.

LC Class. No.: QB495-500.269

Dewey Class. No.: 520

Trajectory Anomalies in Interplanetary Spacecraft = A Method for Determining Accelerations Due to Thermal Emissions and New Mission Proposals /
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