SBIR/STTR Research Award

Variable View Factor Two-Phase Radiator

Award identifier ab80632e08750bf61d05ccb358d132e1d9cbf5cc3b8e3bbb618e2e2d43b783b4Awarding agency National Aeronautics and Space Administration

Award amount

$748,848

Program and phase

SBIR · Phase II

Award year

2019

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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
2019-07-08
Contract end date
2021-07-07
UEI
Z8KVZV3DR7J4
Solicitation number
SBIR_18_P2
Topic code
Z2

Research abstract

The proposed program will develop a novel Vapor-Pressure-Driven Variable-View-Factor Radiator that is deployable, operates with variable geometry (i.e., form factor) and offers high turndown ratio. The device utilizes two-phase heat transfer and novel geometric features that adaptively (and reversibly) adjust the view factor in response to internal pressure in the radiator. The radiator folds into a closed shape to minimize the view factor when cold, and opens up to maximize the view factor when heated. Prototypes demonstrated in Phase I prove the feasibility and highlight the advantages of a two-phase radiator over shape memory alloy technologies.nbsp; Structural and thermal simulation studies confirmed the viability of the concept.At low temperatures, the view factor of emissive surfaces of the radiator to the heat sink is near zero, so the only heat lost is that which is emitted from the insulated outer surfaces of the radiator. The flexible section of the radiator is an elastic envelope enclosing a saturated working fluid. When the temperature of the radiator increases, the corresponding increase in vapor pressure generates a net force on the interior walls of the envelope which causes the elastic walls to bend so that the structure opens and the view factor increases. The increase in view factor reduces thermal resistance of heat rejection which enables inherently passive thermal control. Additionally, the entire structure of the radiator consists of cavities filled with saturated fluid acting like heat pipes, so the radiating surface will be nearly isothermal, achieving a radiator panel efficiency near one. In Phase I, modeling and prototyping indicates that the baseline geometry proposed can achieve a thermal turndown ratio of 37:1.

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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