The geometric form of a space station is presented that includes a description of a plurality of modules and berthing hubs, joined by interconnections which are sideways connectable. The modules and hubs are fastened together in a triangular configuration in three dimensions. The interconnections include a pair of opposed, axially aligned, flanged ports and a clamp latch formed from a plurality of sections hinged along their length and extending circumferentially around the flanged ports. A hermetic seal is formed between the ports. A utilities connection channel extends between the ports. The channel has a shell with utilities connectors movable between an extended position to mating connectors in the modules and a withdrawn position. Assembly sequence and common module shell structure is detailed.
Space Station Architecture, Module, Berthing Hub, Shell Assembly, Berthing Mechanism and Utility Connection Channel
1984
25 pages
Report
No indication
English
Manned Spacecraft , Mechanical Devices & Equipment , Patent applications , Controlled atmospheres , Geometry , Space shuttle payloads , Space stations , Spacecraft configurations , Spacecraft design , Spacecraft docking , Spacecraft electronic equipment , Environmental engineering , Hubs , Spacecraft control , Spacecraft environments , Spacecraft modules
Space Station Freedom Common Berthing Mechanism
NTIS | 1992
|Space Station Freedom common berthing mechanism
NTRS | 1992
|