Orbit design for launching INTEGRAL on the Proton/Block-DM launcher

被引：32

作者：

Eismont, NA

Ditrikh, AV

Janin, G

Karrask, VK

Clausen, K

Medvedchikov, AI

Kulik, SV

Vtorushin, NA

Yakushin, NI

机构：

[1] Russian Acad Sci, Space Res Inst, Moscow 117907, Russia

[2] Rocket & Space Corp Energia, Korolev, Russia

[3] ESA, ESOC, D-64293 Darmstadt, Germany

[4] Khrunichev State Res & Product Space Ctr, Moscow, Russia

[5] ESA, Estec, NL-2201 AZ Noordwijk, Netherlands

[6] Rosaviacosmos, Moscow 129857, Russia

来源：

ASTRONOMY & ASTROPHYSICS | 2003年 / 411卷 / 01期

关键词：

space vehicles; orbit evolution; launch window;

D O I：

10.1051/0004-6361:20031452

中图分类号：

P1 [天文学];

学科分类号：

0704 ;

摘要：

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.

引用

页码：L37 / L41

页数：5