| 000 | 03272nam a22005055i 4500 | ||
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| 001 | vtls000559968 | ||
| 003 | RU-ToGU | ||
| 005 | 20210922090058.0 | ||
| 007 | cr nn 008mamaa | ||
| 008 | 170212s2015 gw | s |||| 0|eng d | ||
| 020 |
_a9783319189802 _9978-3-319-18980-2 |
||
| 024 | 7 |
_a10.1007/978-3-319-18980-2 _2doi |
|
| 035 | _ato000559968 | ||
| 040 |
_aSpringer _cSpringer _dRU-ToGU |
||
| 050 | 4 | _aQB495-500.269 | |
| 072 | 7 |
_aTTDS _2bicssc |
|
| 072 | 7 |
_aSCI005000 _2bisacsh |
|
| 082 | 0 | 4 |
_a520 _223 |
| 082 | 0 | 4 |
_a500.5 _223 |
| 100 | 1 |
_aFrancisco, Frederico. _eauthor. _9466730 |
|
| 245 | 1 | 0 |
_aTrajectory Anomalies in Interplanetary Spacecraft _helectronic resource _bA Method for Determining Accelerations Due to Thermal Emissions and New Mission Proposals / _cby Frederico Francisco. |
| 260 |
_aCham : _bSpringer International Publishing : _bImprint: Springer, _c2015. |
||
| 300 |
_aXVII, 87 p. 27 illus., 3 illus. in color. _bonline resource. |
||
| 336 |
_atext _btxt _2rdacontent |
||
| 337 |
_acomputer _bc _2rdamedia |
||
| 338 |
_aonline resource _bcr _2rdacarrier |
||
| 490 | 1 |
_aSpringer Theses, Recognizing Outstanding Ph.D. Research, _x2190-5053 |
|
| 505 | 0 | _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. | |
| 520 | _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. | ||
| 650 | 0 |
_aphysics. _9566227 |
|
| 650 | 0 |
_aSpace sciences. _9460714 |
|
| 650 | 0 |
_aAerospace engineering. _9460709 |
|
| 650 | 0 |
_aAstronautics. _9303158 |
|
| 650 | 1 | 4 |
_aPhysics. _9566228 |
| 650 | 2 | 4 |
_aExtraterrestrial Physics, Space Sciences. _9303573 |
| 650 | 2 | 4 |
_aTheoretical, Mathematical and Computational Physics. _9410498 |
| 650 | 2 | 4 |
_aAerospace Technology and Astronautics. _9304214 |
| 710 | 2 |
_aSpringerLink (Online service) _9143950 |
|
| 773 | 0 | _tSpringer eBooks | |
| 830 | 0 |
_aSpringer Theses, Recognizing Outstanding Ph.D. Research, _9567110 |
|
| 856 | 4 | 0 | _uhttp://dx.doi.org/10.1007/978-3-319-18980-2 |
| 912 | _aZDB-2-PHA | ||
| 999 | _c414729 | ||