This paper discusses an application of multi-body dynamic analysis conducted at the Boeing Company in connection with the Space Station (SS) Common Berthing Mechanism (CBM). After introducing the hardware and analytical objectives we will focus on some of the day-to-day computational issues associated with this type of analysis.
Space Station Common Berthing Mechanism, a Multi-Body Simulation Application
1993
14 pages
Report
No indication
English
Space Station Freedom common berthing mechanism
NTRS | 1992
|Space Station Freedom Common Berthing Mechanism
NTIS | 1992
|The Common Berthing Mechanism (CBM) for International Space Station
SAE Technical Papers | 2001
|The Common Berthing Mechanism (CBM) for International Space Station
British Library Conference Proceedings | 2001
|