Generation of simplified spacecraft mathematical models with equivalent dynamic characteristics for launcher/spacecraft coupled dynamic loads analysis
31st Structures, Structural Dynamics and Materials Conference ; 1990 ; Long Beach , CA , U.S.A.
01.01.1990
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Generation of Simplified Spacecraft Mathematical Models with Equivalent Dynamic Characteristics
Online Contents | 1995
|SPACECRAFT ON-ORBIT COUPLED LOADS ANALYSIS
AIAA | 1993
|Spacecraft on-orbit coupled loads analysis
NTRS | 1993
|Affordable Launcher for Small Spacecraft Missions
British Library Conference Proceedings | 2001
|