Common Berthing Mechanism - Wikipedia
The Common Berthing Mechanism (CBM) connects habitable elements in the US Orbital Segment (USOS) of the International Space Station (ISS). The CBM has two distinct sides that, once mated, form a cylindrical vestibule between modules. The vestibule is about 16 inches (0.4 m) long and 6 feet (1.8 m) across.
空间对接 - 维基百科，自由的百科全书
在其后的 阿波罗计划 中，航天员在登陆月球前后需要至少两次在阿波罗指令/服务舱（CSM）和登月舱（LM）之间进行人员转移和撤离，而空间交会对接作为 航天员 在指令/服务舱和 登月舱 间进行转移时的重要步骤而被极其重视 [14]。 在一次标准的阿波罗登月任务中，飞船在被送入地月转移轨道不久后指令/服务舱就需首先与火箭的第三级分离，然后与登月舱进行空间对接，将其从火箭中抽出并撤离 [15][16]。 其后航天员在完成登月任务并驾驶登月舱上升段起飞后，上升段上的两 …
Space Station Freedom common berthing mechanism - NASA …
1992年5月1日 · The Common Berthing Mechanism (CBM) is a generic device used to join the pressurized elements of the Space Station Freedom (SSF) utilizing the Space Shuttle Orbiter Remote Manipulator System (SRMS) or the Space …
Berthing and deberthing of two elements together on-orbit occurs many times throughout the Space Station Assembly Sequence to provide pressurized access between the module vestibules via hatches.
The Common Berthing Mechanism (CBM) was used on the ISS as the primary connection between pressurized elements on the US segment. As the name implies, the CBM is a berthing system instead of a docking system.
The Common Berthing Mechanism (CBM) for International Space Station
2001年7月9日 · The International Space Station (ISS) Program utilizes the Common Berthing Mechanism (CBM) hardware to mate/berth or demate/deberth two pressurized elements on-orbit. Berthing and deberthing of two elements together on-orbit occurs many times throughout the Space Station Assembly Sequence to provide
Space Station Freedom common berthing mechanism
1992年5月1日 · The Common Berthing Mechanism (CBM) is a generic device used to join the pressurized elements of the Space Station Freedom (SSF) utilizing the Space Shuttle Orbiter Remote Manipulator System (SRMS) or the Space …
How are hatches set up in the common berthing mechanism (CBM)?
I have read about the common berthing mechanism on ISS and how the attachment process works and how the pressure seal is established, and I think I have that part figured out. There is a passive CBM and an active CBM which mate together and provide a pressure tight seal against space around them.
Towards the construction of the inner zone of the CBM-TOF wall - NASA…
Our R&D activity has been focused on the development of a MSMGRPC prototype for the most demanding region of the CBM-TOF wall, the region of low polar angles (from 2.5° to ∼12° around the beam pipe).
The Common Berthing Mechanism (CBM) for International
2001年7月9日 · The CBM system was developed by Boeing at Marshall Space Flight Center (MSFC) in Huntsville, Alabama, under contract to NASA, and the CBM Control and Actuation Components were developed by ...