One of the most critical operational functions for the space station is the orbital docking between the station and the STS orbiter. The program to design, fabricate, and test docking/berthing mechanisms for the space station is described. The design reflects space station overall requirements and consists of two mating docking mechanism halves. One half is designed for use on the shuttle orbiter and incorporates capture and energy attenuation systems using computer controlled electromechanical actuators and/or attenuators. The mating half incorporates a flexible feature to allow two degrees of freedom at the module-to-module interface of the space station pressurized habitat volumes. The design concepts developed for the prototype units ma...
The objective of the STRONG mission is the deployment of payloads from Low Earth Orbit into greater ...
Design and fabricate test hardware for NASA's George C. Marshall Space Flight Center (MSFC) are repo...
TRW has conducted an extensive Contact Dynamics Test Program (CDTP) of the Three Point Docking Mecha...
Conceptual efforts to develop a Space Station based system for docking and/or berthing the NSTS Orbi...
A prototype docking mechanism for the Space Station was designed and fabricated for NASA. This docki...
The Space Station/Space Operations Mechanism Test Bed consists of the following: a hydraulically dri...
A mechanism is disclosed for the docking of a spacecraft to a space station where a connection for t...
This paper discloses the design procedure of a docking mechanism for space applications. The mechani...
The development of a docking system for aerospace vehicles has identified the need for reusable and ...
A system is presented for docking a space vehicle to a space station where a connecting tunnel for i...
As space vehicles and structures become larger and more complex, the development of systems to assis...
The primary purpose of the OMV is to dock with orbiting payloads and then either transfer them to a ...
Docking mechanisms have been employed in space missions for more than 50 years. In fact, since the A...
The opening, closing, and latching of the first large clamshell door to operate in space presented s...
This dissertation addresses the design procedure of a docking mechanism for space applications, in p...
The objective of the STRONG mission is the deployment of payloads from Low Earth Orbit into greater ...
Design and fabricate test hardware for NASA's George C. Marshall Space Flight Center (MSFC) are repo...
TRW has conducted an extensive Contact Dynamics Test Program (CDTP) of the Three Point Docking Mecha...
Conceptual efforts to develop a Space Station based system for docking and/or berthing the NSTS Orbi...
A prototype docking mechanism for the Space Station was designed and fabricated for NASA. This docki...
The Space Station/Space Operations Mechanism Test Bed consists of the following: a hydraulically dri...
A mechanism is disclosed for the docking of a spacecraft to a space station where a connection for t...
This paper discloses the design procedure of a docking mechanism for space applications. The mechani...
The development of a docking system for aerospace vehicles has identified the need for reusable and ...
A system is presented for docking a space vehicle to a space station where a connecting tunnel for i...
As space vehicles and structures become larger and more complex, the development of systems to assis...
The primary purpose of the OMV is to dock with orbiting payloads and then either transfer them to a ...
Docking mechanisms have been employed in space missions for more than 50 years. In fact, since the A...
The opening, closing, and latching of the first large clamshell door to operate in space presented s...
This dissertation addresses the design procedure of a docking mechanism for space applications, in p...
The objective of the STRONG mission is the deployment of payloads from Low Earth Orbit into greater ...
Design and fabricate test hardware for NASA's George C. Marshall Space Flight Center (MSFC) are repo...
TRW has conducted an extensive Contact Dynamics Test Program (CDTP) of the Three Point Docking Mecha...