SLIDE 3
– Fully developed flow in radiator (hydraulic and thermal) – System temperature drop, heat load, and radiator geometry held constant – Fluid temperature range based on potential mission profiles
Design Criteria
300 250 200 150 100 50
Sink Temperature (K)
6000 5000 4000 3000 2000 1000
Heat Rejection (W) Sink Temperature Heat Rejection
0 50 100 150 200 250 300 350 400
Mission Elapsed Time (hr)
Cognata, T.J., Hartl, D.J., Sheth, R., and C. Dinsmore. "A Morphing Radiator for High- Turndown Thermal Control of Crewed Space Exploration Vehicles", 23rd AIAA/AHS Adaptive Structures Conference, AIAA SciTech, (AIAA 2015-1509)
– Pumping ability: – Heat transfer: – Pump work:
base f
k k
20 90
base f f p base p
c c
2 67 . 33 . 5 .
base f base f f base
k k
Laminar Turbulent Laminar
TFAWS 2017 – August 21-25, 2017
3