|
Goddard
Space Flight Center
1992 Phase II
Cryogenic
Heat Transport System
Cullimore
& Ring Technologies
Littleton, CO
Swales
and Associates
Beltsville, MD
|
INNOVATION
A vibration isolating
cryogenic heat transport system capable of transporting waste heat from
electronics and sensors over long distances with the use of no moving
parts or thermal switches.
|
Cryogenic Heat Transport System
Optional Powerpoint
file
|
|
ACCOMPLISHMENTS
- The technology successfully
operated at 80-90 °K during ground tests and in the zero gravity
CRYOTSU canister on board STS-95
- Testing successfully demonstrated
acquisition of waste heat through the vaporization of a working
fluid which is passively pumped using the surface tension forces
developed in a fine porous wick structure
- Extrapolated the development
of similar room temperature technology to cryogenic applications
- Characterized operation for
an 80-90 °K system using nitrogen as the working fluid. Spin
off development demonstrated functionality down to 40 °K using
neon.
|
COMMERCIALIZATION
- Miniaturization of loop components
has provided the ground work for extrapolating the technology to
room temperature electronic cooling.
|
GOVERNMENT/SCIENCE
APPLICATIONS
- Vibration free cooling
of cryogenic sensors and electronics
- Method for connecting
multiple cryogenic cooling sources to a single heat source
- Lightweight, flexible,
vibration free
replacement for cryogenic
thermal switches
|
| For more
information about this firm, please send e-mail to crtech
or Swales representatives
Return
to NASA SBIR Success Listings
|
Curator:
SBIR Support |