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

Astronomy and Astrophysics

Volumn 411, Issue 1, 2003, Pages

  Eismont, N A ^a   Ditrikh, A V ^b   Janin, G ^c   Karrask, V K ^d   Clausen, K ^e   Medvedchikov, A I ^f   Kulik, S V ^f   Vtorushin, N A ^f   Yakushin, N I ^f  

^a Russian Academy of Sciences ^*  (Russian Federation)

^b S P KOROLEV ROCKET AND SPACE CORPORATION ENERGIA   (Russian Federation)

^c ESA ESOC   (Germany)

^d Khrunichev State Research and Production Space Center   (Russian Federation)

^e EUROPEAN SPACE AGENCY   (Netherlands)

^f KELDYSH RESEARCH CENTER   (Russian Federation)

Author keywords

Launch window; Orbit evolution; Space vehicles

Indexed keywords

GAMMA RAYS; LAUNCHING; ORBITS; RADIO ASTRONOMY; SPACECRAFT OBSERVATORIES;

GAMMA-RAY ASTRONOMY;

ASTROPHYSICS;

EID: 0242661891     PISSN: 00046361     EISSN: None     Source Type: Journal    
DOI: 10.1051/0004-6361:20031452     Document Type: Article

References (5)

1. Eismont, N., Khrapchenkov, V., Janin, G., & Mugelessi-Dow, R. 2003, Design of High Elliptical and Distant Earth Connected Trajectories, in Proc. of 17th Symp. on Space Flight Dynamics, Moscow, June 16-20, 2003, to be published
2. Eliasberg, P. E. 1965, Introduction to the Theory of Flight of Artificial Earth Satellites (in Russian), Moscow, Nauka, 491
3. Janin, G. 2001, INTEGRAL on Proton CreMA for the 72-h Orbit, INT-RP-2272, ESOC, Darmstadt
4. Janin, G. 2002, INTEGRAL Orbits with 9000 km Initial Perigee Height, MAO Technical Note No. 36. INT-MOC-MA-RP-1001-TOS-GA, ESOC, Darmstadt, October 2002
5. Proton Launch Vehicle and Launch Services User's Guide 1995, International Launch Services, San Diego, Rev. 2, Issue 1, December 1995