000 | 02123cam a2200457 i 4500 | ||
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003 | OCoLC | ||
005 | 20221101225811.0 | ||
008 | 130516s2014 enka b 001 0 eng d | ||
010 | _a 2014397914 | ||
011 | _aMARC Score : 11000(22700) : OK | ||
011 | _aDirect Search Result | ||
011 | _aBIB MATCHES WORLDCAT | ||
020 |
_a0080977472 _qhbk. |
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020 |
_a9780080977478 _qhbk. |
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035 | _a(ATU)b14918286 | ||
035 | _a(OCoLC)852806044 | ||
040 |
_aUKMGB _beng _erda _cUKMGB _dOCLCO _dYDXCP _dXII _dIXA _dQCL _dCUD _dDLC _dOCLCF _dGBVCP _dOCLCQ _dATU |
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050 | 4 |
_aTL1050 _b.C87 2014 |
|
082 | 0 | 4 |
_a629.4113 _223 |
099 | _a629.4113 CUR | ||
100 | 1 |
_aCurtis, Howard D., _eauthor. _9839497 |
|
245 | 1 | 0 |
_aOrbital mechanics for engineering students / _cHoward D. Curtis, Professor of Aerospace Engineering, Embry-Riddle Aeronautical University, Daytona Beach, Florida. |
250 | _aThird edition. | ||
264 | 1 |
_aOxford, UK : _bElsevier, Butterworth-Heinemann is an imprint of Elsevier, _c[2014] |
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264 | 4 | _c©2014 | |
300 |
_axiii, 751 pages : _billustrations ; _c25 cm. |
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336 |
_atext _btxt _2rdacontent |
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337 |
_aunmediated _bn _2rdamedia |
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338 |
_avolume _bnc _2rdacarrier |
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490 | 1 | _aElsevier aerospace engineering series | |
500 | _aPrevious edition: 2010. | ||
504 | _aIncludes bibliographical references and index. | ||
505 | 0 | _aDynamics of point masses -- The two-body problem -- Orbital position as a function of time -- Orbits in three dimensions -- Preliminary orbit determination -- Orbital maneuvers -- Relative motion and rendezvous -- Interplanetary trajectories -- Rigid body dynamics -- Satellite attitude dynamics -- Rocket vehicle dynamics -- Introduction to orbital perturbations. | |
650 | 0 |
_aOrbital mechanics. _9341593 |
|
776 | 1 | 8 |
_w(OCoLC)838792000 _w(OCoLC)868127302 |
830 | 0 |
_aElsevier aerospace engineering series. _91064964 |
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907 |
_a.b14918286 _b11-08-17 _c11-04-16 |
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942 | _cB | ||
945 |
_a629.4113 CUR _g1 _iA547059B _j0 _lcmain _o- _p$141.93 _q- _r- _s- _t0 _u5 _v3 _w2 _x3 _y.i13499683 _z14-06-16 |
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998 |
_ab _ac _b14-06-16 _cm _da _feng _genk _h0 |
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999 |
_c1305138 _d1305138 |