A launch strategy for high-inclination orbit missions from the San Marco equatorial range
Congress; 48th, International Astronautical Federation ; 1997 ; Turin; Italy
International Astronautical Federation ; 4/10 ; 559-568
ACTA ASTRONAUTICA ; 41 , 4/10
01.01.1997
10 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
A launch strategy for high-inclination orbit missions from the San Marco equatorial range
Online Contents | 1997
|History of the Italian San Marco Equatorial Mobile Range
NTIS | 1971
|A guidance algorithm for launch to equatorial orbit
Online Contents | 2009
|A guidance algorithm for launch to equatorial orbit
Emerald Group Publishing | 2009
|Minimum lunar orbit inclination to lunar equatorial plane for earth-launched vehicle
Engineering Index Backfile | 1964
|