Project Title:
A miniature, self-regulating heat switch based on paraffin technology
94-1 08.05 6707
A miniature, self-regulating heat switch based on paraffin
technology
Abstract:
A self-regulating miniature heat switch based on the phase change
properties of paraffin is proposed. This innovation will provide
passive, autonomous temperature regulation to spaceflight micro-
instruments and electronics packages. The objectives of this
project are to determine the specification and design of a
paraffin heat switch, fabricate a "proof-of-principle" unit,
perform validation testing, and evaluate the test results. It is
anticipated that validation tests will confirm the paraffin heat
switch as a viable means of providing autonomous. stable
temperature regulation through proportional conductivity. It is
also anticipated that the "proof-of-principle" design will
inherently lend its self to miniaturization and optimization
during a phase 11 effort to develop a commercially producible,
flight qualified product offering stability and self-regulation
in a small, light package. This level of miniaturization opens
the door to a new field of instrument mounts and thermal strap
terminations which incorporate this technology without
significant size increase. These devices will be utilized on the
new generation of micro-instruments which require thermal
stability to achieve enhanced capability, accuracy, and fidelity.
These instruments will be deployed on NASA small-sats and micro-
sats which which rely on the simple operation and light-weighting
of their payloads to perform missions "faster, better, and
cheaper".
The market niche for smart materials thermal switches has emerged
through the evolution of spacecraft instrument and electronics
design in conjunction with a significant shift in spacecraft
design. This niche is projected to expand rapidly as the trend
towards small satellites and micro satellites with sophisticated
and sensitive payloads continues. This shift is being seen not
only in NASA, but in military and commercial space as well.
Terrestrial applications for this device would include thermal
control of small instruments or electronics packages where
thermal stability allows for optimum performance. This may prove
particularly valuable for use in harsh environments not conducive
to more traditional thermostatic approaches such as vacuum
chambers.
Key words
Starsys Research Corporation
5757 Central Avenue, Suite E
Boulder, CO 80301