SBIR/STTR Research Award

Advanced Hot Reservoir Variable Conductance Heat Pipes for Planetary Landers

Award identifier d309697f62c604a07da4b344ff3e15cf130cccde262a3d49045625199e47a1b8Awarding agency National Aeronautics and Space Administration

Award amount

$749,998

Program and phase

STTR · Phase II

Award year

2020

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
ADVANCED COOLING TECHNOLOGIES INC
Proposal award date
2019-12-19
Contract end date
2021-12-18
UEI
Z8KVZV3DR7J4
Solicitation number
STTR_18_P2
Topic code
T9

Research abstract

NASArsquo;s plans to further expand human and robotic presence in space and planetary surface automatically involve significant thermal challenges. A hot reservoir variable conductance heat pipe (VCHP) that can provide much tighter passive thermal control capability is an ideal thermal management device for future planetary landers and rovers. Based on previous ISS test results, advanced fluid management features and strategies are the key to maximize hot reservoir VCHPrsquo;s reliability during long-term planetary exploration missions. In STTR Phase I, Advanced Cooling Technologies, Inc. (ACT) in collaboration with Case Western Reserve University (CWRU) performed a fundamental study to understand the complex fluid transport phenomena within a hot reservoir VCHP. A Loop Hot Reservoir VCHP (LHR-VCHP) concept was devised during the program. With the novel loop configuration, two mechanisms to induce a net transport flow for VCHP purging (i.e. removal of working fluid from the reservoir) were identified: (1) by momentum transfer from vapor to NCG through shearing (2) by filtering the pulses (via a Tesla/check valve) generated in the heat pipe section of VCHP loop. The existence of momentum transfer flow and its effectiveness on VCHP reservoir purging were demonstrated through modeling and experiment. In Phase II, ACT-CWRU team proposes to further mature the LHR-VCHP technology and demonstrate its reliability by maximizing the flow rate induced by the two mechanisms stated above. Phase II work plan will include systematic studies of both momentum transfer induced flow and pulses generation and filtering induced flow within a loop VCHP, development of fluid diodes for pulses filtration, design and optimization of LHR-VCHP prototypes based on the two mechanisms. At the end of the program, a prototype-flight LHR-VCHP for planetary landers and rovers thermal management will be developed based on the best solution that potentially could result from both mechanisms combined.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Research funding history

282 SBIR/STTR records share this UEI (2003–2026). Reported award amounts total $118,415,811. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Energy, National Science Foundation, Department of Agriculture, Department of Health and Human Services

Agency intelligence

National Aeronautics and Space Administration

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