Three generic types of structural concepts and nonstructural surface densities were selected and combined to represent potential LSS applications. The design characteristics of various classes of large space systems that are impacted by primary propulsion thrust required to effect orbit transfer were identified. The effects of propulsion system thrust-to-mass ratio, thrust transients, and performance on the mass, area, and orbit transfer characteristics of large space systems were determined.
Primary propulsion/large space system interactions
01.07.1980
Aufsatz (Konferenz)
Keine Angabe
Englisch
Primary Propulsion/Large Space System Interaction Study
NTIS | 1981
|Primary propulsion/large space system interaction study
NTRS | 1981
|Large Space Systems/Propulsion Interactions
NTRS | 1982
Large Space Systems/Propulsion Interactions
NTIS | 1982
Overview of large space systems/propulsion interactions
NTRS | 1982
|