Two latches were designed to mount payloads in the shuttle orbiter bay. Multiple retention latches attach a payload to the sill longerons and another latch device attaches it to the keel. Requirements for each actuator are defined and drive mechanisms are described. Other design aspects discussed include: switch mechanisms, motors, gearboxes, redundancy provisions, structural materials, and lubricants. A preliminary dry lubricant test program is also reviewed and results presented.
Payload retention latches for the shuttle orbiter
01.05.1981
Aufsatz (Konferenz)
Keine Angabe
Englisch
The Space Shuttle orbiter payload retention systems
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