Title of article
Orbit design for launching INTEGRAL on the Proton/Block-DM launcher
Author/Authors
Eismont، N. A. نويسنده , , Clausen، K. نويسنده , , Janin، G. نويسنده , , Ditrikh، A. V. نويسنده , , Karrask، V. K. نويسنده , , Medvedchikov، A. I. نويسنده , , Kulik، S. V. نويسنده , , Vtorushin، N. A. نويسنده , , Yakushin، N. I. نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2003
Pages
-36
From page
37
To page
0
Abstract
This paper describes some aspects of the mission design determined by use of the Proton/Block-DM launch vehicle in the version used for injection onto a highly elliptical orbit of the international gamma-ray astrophysics laboratory INTEGRAL. Methods and results used for choosing an operational orbit for INTEGRAL are presented.
Keywords
space vehicles , orbit evolution , launch window
Journal title
Astronomy and Astrophysics
Serial Year
2003
Journal title
Astronomy and Astrophysics
Record number
77998
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