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A Two-Phase Pumped Loop Evaporator with Adaptive Flow Distribution for Large Area Cooling

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: 80NSSC18C0060
Agency Tracking Number: 175050
Amount: $749,966.00
Phase: Phase II
Program: SBIR
Solicitation Topic Code: S3
Solicitation Number: SBIR_17_P2
Timeline
Solicitation Year: 2017
Award Year: 2018
Award Start Date (Proposal Award Date): 2018-05-08
Award End Date (Contract End Date): 2020-05-07
Small Business Information
16 Great Hollow Road, Hanover, NH, 03755-3116
DUNS: 072021041
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Weibo Chen
 (603) 640-2425
 wbc@creare.com
Business Contact
 Sheryl Belanger
Phone: (603) 643-3800
Email: contractsmgr@creare.com
Research Institution
N/A
Abstract

NASA’s future remote sensing science missions require advanced thermal management technologies to maintain multiple instruments at very stable temperatures and utilize waste heat to keep other critical subsystems above minimum operational temperatures. Two-phase pumped loops are an ideal solution for these applications. A critical need for these pumped loops is a microgravity-compatible evaporator having a large cooling area to maintain the temperatures of multiple electronics and instruments. The evaporator must be able to accommodate multiple heat loads with a wide range of heat flux densities and allow heat loads to be mounted on any available locations of its cooling surfaces to facilitate vehicle-level system integration. To this end, Creare proposes to develop a lightweight, compact evaporator with innovative internal design features to adaptively distribute liquid refrigerant to heated areas, preventing dryout in areas with high heat flux. This advanced flow distribution feature reduces liquid recirculation flow in the pumped loop and thus the system power input. The design features also provide strong internal structural support for the evaporator, reducing the size and mass of the evaporator cover plates. In Phase I, we proved the feasibility of the evaporator by developing a preliminary evaporator design, predicting its overall performance, and demonstrating its key performance features and fabrication processes by testing. In Phase II, we will optimize the evaporator design, fabricate a 0.5 m x 0.5 m evaporator, demonstrate its steady state and transient performance in a representative pumped loop, and deliver it to NASA JPL for further performance evaluation.

* Information listed above is at the time of submission. *

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