The centerline latch tool was designed and developed as an EVA manual backup device for latching the Space Shuttle Orbiter's payload bay doors for reentry in case of a failure of the existing centerline latches to operate properly. The tool was designed to satisfy a wide variety of structural, mechanical, and EVA requirements. It provides a load path for forces on the payload bay doors during reentry. Since the tool would be used by an EVA crewmember, control, handgrips, operating forces, and procedures must be within the capabilities of a partially restrained, suited crewmember in a zero-gravity environment. The centerline latch tool described was designed, developed, and tested to meet these requirements
One of the most critical operational functions for the space station is the orbital docking between ...
Latching techniques are changing from early approaches due to the advent of berthing technology. Lat...
The orbiter elevon seal panel mechanism controls the position of fairing panels between the orbiter ...
The opening, closing, and latching of the first large clamshell door to operate in space presented s...
A latching mechanism in which there is linear movement and rotational movement is described. The umb...
The Starlab Experiment, a major SDIO technology initiative, is an attached payload which will be del...
The device described in this paper is a modular hinge latch mechanism. It is used to latch and prelo...
Bodies/systems need to be stopped and locked/latched at the end of their path. Some examples of thes...
The Latching End Effector (LEE) forms part of the Space Station Remote Manipulator System (SSRMS) fo...
The primary purpose of the OMV is to dock with orbiting payloads and then either transfer them to a ...
The requirements, design tradeoff, design, and performance of the Spacelab scientific airlock hatch ...
Latching mechanism that is securely locked by the movement of the operating handle in one direction ...
An apparatus for securing payloads in a space vehicle such as the space shuttle is described. The ap...
Double hook latch provides preloading and support capability up to 80,000 pounds and opens self-ener...
The design, assembly, and test processes followed in developing a space-qualified aperture door syst...
One of the most critical operational functions for the space station is the orbital docking between ...
Latching techniques are changing from early approaches due to the advent of berthing technology. Lat...
The orbiter elevon seal panel mechanism controls the position of fairing panels between the orbiter ...
The opening, closing, and latching of the first large clamshell door to operate in space presented s...
A latching mechanism in which there is linear movement and rotational movement is described. The umb...
The Starlab Experiment, a major SDIO technology initiative, is an attached payload which will be del...
The device described in this paper is a modular hinge latch mechanism. It is used to latch and prelo...
Bodies/systems need to be stopped and locked/latched at the end of their path. Some examples of thes...
The Latching End Effector (LEE) forms part of the Space Station Remote Manipulator System (SSRMS) fo...
The primary purpose of the OMV is to dock with orbiting payloads and then either transfer them to a ...
The requirements, design tradeoff, design, and performance of the Spacelab scientific airlock hatch ...
Latching mechanism that is securely locked by the movement of the operating handle in one direction ...
An apparatus for securing payloads in a space vehicle such as the space shuttle is described. The ap...
Double hook latch provides preloading and support capability up to 80,000 pounds and opens self-ener...
The design, assembly, and test processes followed in developing a space-qualified aperture door syst...
One of the most critical operational functions for the space station is the orbital docking between ...
Latching techniques are changing from early approaches due to the advent of berthing technology. Lat...
The orbiter elevon seal panel mechanism controls the position of fairing panels between the orbiter ...