LEADER 04055nam 22006975 450 001 9910300417803321 005 20200705071209.0 010 $a3-319-18980-8 024 7 $a10.1007/978-3-319-18980-2 035 $a(CKB)3710000000422037 035 $a(EBL)2120648 035 $a(OCoLC)910662606 035 $a(SSID)ssj0001524763 035 $a(PQKBManifestationID)11918833 035 $a(PQKBTitleCode)TC0001524763 035 $a(PQKBWorkID)11484882 035 $a(PQKB)10213630 035 $a(DE-He213)978-3-319-18980-2 035 $a(MiAaPQ)EBC2120648 035 $a(PPN)186401469 035 $a(EXLCZ)993710000000422037 100 $a20150602d2015 u| 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 10$aTrajectory Anomalies in Interplanetary Spacecraft $eA Method for Determining Accelerations Due to Thermal Emissions and New Mission Proposals /$fby Frederico Francisco 205 $a1st ed. 2015. 210 1$aCham :$cSpringer International Publishing :$cImprint: Springer,$d2015. 215 $a1 online resource (98 p.) 225 1 $aSpringer Theses, Recognizing Outstanding Ph.D. Research,$x2190-5053 300 $aDescription based upon print version of record. 311 $a3-319-18979-4 320 $aIncludes bibliographical references at the end of each chapters. 327 $aIntroduction -- 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. 330 $aThis thesis presents fundamental work that explains two mysteries concerning the trajectory of interplanetary spacecraft. For the first problem, the so-called Pioneer anomaly, a wholly new and innovative method was developed for computing all contributions to the acceleration due to onboard thermal sources. Through a careful analysis of all parts of the spacecraft Pioneer 10 and 11, the application of this methodology has yielded the observed anomalous acceleration. This marks a major achievement, given that this problem remained unsolved for more than a decade. For the second anomaly, the flyby anomaly, a tiny glitch in the velocity of spacecraft that perform gravity assisting maneuvers on Earth, no definitive answer is put forward; however a quite promising strategy for examining the problem is provided and a new mission is proposed. The proposal largely consists in using the Galileo Navigational Satellite System to track approaching spacecraft, and in considering a small test body that approaches Earth from a highly elliptic trajectory. 410 0$aSpringer Theses, Recognizing Outstanding Ph.D. Research,$x2190-5053 606 $aSpace sciences 606 $aMathematical physics 606 $aAerospace engineering 606 $aAstronautics 606 $aSpace Sciences (including Extraterrestrial Physics, Space Exploration and Astronautics)$3https://scigraph.springernature.com/ontologies/product-market-codes/P22030 606 $aTheoretical, Mathematical and Computational Physics$3https://scigraph.springernature.com/ontologies/product-market-codes/P19005 606 $aAerospace Technology and Astronautics$3https://scigraph.springernature.com/ontologies/product-market-codes/T17050 615 0$aSpace sciences. 615 0$aMathematical physics. 615 0$aAerospace engineering. 615 0$aAstronautics. 615 14$aSpace Sciences (including Extraterrestrial Physics, Space Exploration and Astronautics). 615 24$aTheoretical, Mathematical and Computational Physics. 615 24$aAerospace Technology and Astronautics. 676 $a629.41 700 $aFrancisco$b Frederico$4aut$4http://id.loc.gov/vocabulary/relators/aut$0792799 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910300417803321 996 $aTrajectory Anomalies in Interplanetary Spacecraft$91773029 997 $aUNINA