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

Saved in:
Bibliographic Details
Author / Creator:Francisco, Frederico, author.
Imprint:Cham : Springer, [2015]
©2015
Description:1 online resource.
Language:English
Series:Springer Theses, Recognizing Outstanding Ph. D. Research, 2190-5053
Springer Theses, Recognizing Outstanding Ph. D. Research,
Subject:
Format: E-Resource Dissertations Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/11094245
Hidden Bibliographic Details
ISBN:9783319189802
3319189808
3319189794
9783319189796
9783319189796
Digital file characteristics:text file PDF
Notes:Includes bibliographical references.
Online resource; title from PDF title page (EBSCO, viewed June 8, 2015).
Summary: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.
Other form:Printed edition: 9783319189796
Standard no.:10.1007/978-3-319-18980-2