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    71. http://hea-www.harvard.edu/~garcia/groot.ps
    ... Time­of­arrival analysis between the Ulysses spacecraft, BeppoSAX and BATSE, allows the construction of an Interplanetary Network (IPN) annulus which intersects the -- 4 -- BeppoSAX WFC camera error box (Hurley et al., ...
    [ Текст ]  Ссылки http://hea-www.harvard.edu/~garcia/groot.ps -- 1199.2 Кб -- 08.02.2011
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    72. Bookmarks
    ... CSR Directory . A Simple Method of Evaluating the Leonid Storm Fluence and Its Impact on Spacecraft . Leonids 2000 . M&TA home page . ...
    [ Сохраненная копия ]  Ссылки http://hea-www.harvard.edu/~pgreen/bookmarks.html -- 591.4 Кб -- 09.04.2016
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    73. http://hea-www.harvard.edu/AstroStat/etc/scma1997_secfkf.pdf
    ... AXAF Data Analysis Challenges 6 the random jitter of the spacecraft and analysis of `split events' may allow sub-pixel imaging. ...
    [ Текст ]  Ссылки http://hea-www.harvard.edu/AstroStat/etc/scma1997_secfkf.pdf -- 227.8 Кб -- 12.09.2008
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    74. http://hea-www.harvard.edu/PINTofALE/papers/d_MM_palermo.ps.gz
    ... a nearby example of a late­type main sequence mass­losing star, its mass loss rate as measured in situ by different spacecraft amounts to only about ё2\Theta10 \Gamma14 M fi /yr---orders of magnitude lower than any direct non­solar measurements or upper ...
    [ Текст ]  Ссылки http://hea-www.harvard.edu/PINTofALE/papers/d_MM_palermo.ps.gz -- 88.0 Кб -- 12.02.2001
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    75. http://hea-www.harvard.edu/AstroStat/astro193/Lee+2011_apj_731_2_126.pdf
    ... However, after considerable exploration, they found this approach unable to capture the complexities of spacecraft calibration, especially at high energies. ...
    [ Текст ]  Ссылки http://hea-www.harvard.edu/AstroStat/astro193/Lee+2011_apj_731_2_126.pdf -- 2913.9 Кб -- 28.01.2015
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    76. http://hea-www.harvard.edu/~garcia/apj.555.477.ps
    ... using custom IDL procedures in several steps : (1) sky coordinates were transformed to grating coor­ dinates by correcting for spacecraft roll ; (2) the location of zeroth order was determined by пtting a pair of one­ dimensional Gaussian proпles ; (3 ...
    [ Текст ]  Ссылки http://hea-www.harvard.edu/~garcia/apj.555.477.ps -- 1112.1 Кб -- 08.02.2011
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    77. http://hea-www.harvard.edu/~bradw/cv/papers/Ross154.pdf
    ... ACA window (with integration time of 4.1 s per frame) as the spacecraft dithered with a period of 707.1 s in pitch and 1000.0 s ...
    [ Текст ]  Ссылки http://hea-www.harvard.edu/~bradw/cv/papers/Ross154.pdf -- 1659.4 Кб -- 17.03.2008
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    78. http://hea-www.harvard.edu/~kim/pap/2004_M81.pdf
    ... For each observation we used the position of the detected sources,4 excluding the nuclear source M81 X-5, to check for possible misalignments of the astrometric frames and to correct for small spacecraft errors; no further alignment was needed. ...
    [ Текст ]  Ссылки http://hea-www.harvard.edu/~kim/pap/2004_M81.pdf -- 504.9 Кб -- 06.12.2010
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    79. http://hea-www.harvard.edu/~bradw/cv/papers/MBM12.pdf
    ... the line yield per charge exchange, i is the charge exchange cross section, and nn0 is the neutral particle density at 10 Earth radii (RE ); rmin is the geocentric distance to the edge of the magnetosphere or the spacecraft position, whichever is farther ...
    [ Текст ]  Ссылки http://hea-www.harvard.edu/~bradw/cv/papers/MBM12.pdf -- 268.1 Кб -- 07.04.2005
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    80. http://hea-www.harvard.edu/~pgreen/Papers/Q2345.ps
    ... We o#set the pointing by 1 in spacecraft Y­coordinate from the Chandra aim point to allow for imag­ ing of any extended emission all within one ACIS node. ...
    [ Текст ]  Ссылки http://hea-www.harvard.edu/~pgreen/Papers/Q2345.ps -- 2124.2 Кб -- 14.09.2005
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