Project Title:
A Telerobotic/EVA Astronaut Compatible Fastener For Small/Medium
Honeybee Robotics
204 Elizabeth Street
New York, NY 10012
93-1 05.07 0661 A Amount Requested $69,968
A Telerobotic/EVA Astronaut Compatible Fastener For Small/Medium
Sized Payloads
Abstract:
Presently, many small and medium sized payload modules are
secured in place with #10 screws. Unfortunately, these screws cross
thread easily and require epoxy to survive launch, rendering small and
medium payloads as non-candidates for on-orbit servicing. An
innovative fastener for payloads is proposed, as an alternative
to #10 screws, to facilitate telerobotic & EVA astronaut on-orbit
servicing. The proposed fastener is tolerant of initial
misalignments yet cannot crossthread; also no lock down epoxy is
required to survive the launch environment. The objectives of
the research are to confirm the predicated performance of the
innovation, determine the practical feasibility of the fastener
and to investigate the space qualification potential of the
innovation.
The proposed effort is to design and fabricate, working
prototypes of the proposed fastener and to fabricate and test a
comprehensive breadboard version of a small payload module for testing robotic
and manual change-out of said module. The offerer expects the
Phase I effort will lead to the production of the proposed
fastener which in turn will foster the development and production of
serviceable small and medium payload modules. The fastener
development will also hasten the introduction of a comprehensive
"fastening" strategy for telerobotic and EVA on-orbit servicing.
Use of the proposed fastener will accelerate cost reducing
maintenance & repair designs for spacecraft and platform
subsystems; designers will be free to develop small serviceable
payload modules and maintenance strategies. The innovation will
also meet rising industrial demand for robot compatible fasteners
and an industrial demand for a vibration resistant fastener not
requiring locktite.
Fastener, non-crossthreading, vibration resistant, on-orbit
serviceable payload modules.