Describes how specifications for the INTELSAT VI spacecraft bus were generated. In early 1980, a conceptual design was developed to verify the feasibility of implementing the INTELSAT VI mission requirements within the lift-off mass and volume constraints of the launch vehicles being considered. A second goal was to generate specifications that were not only realistic, but also more general than those applicable solely to the baseline design.
Specifying the spacecraft bus
Spezifikation des Intelsat VI-Trägers
Comsat Technical Review ; 20 , 2 ; 309-333
1990
25 Seiten, 7 Quellen
Aufsatz (Zeitschrift)
Englisch
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