SBIR/STTR Research Award

Modular Membrane Controlled Three-phase Deployable Radiator (MMC-TDR)

Award identifier 33d0f4e154ab3d9cb3109ee97c738ef389e14c9754faf2a3a558349fc0451f3fAwarding agency National Aeronautics and Space Administration

Award amount

$124,948

Program and phase

SBIR · Phase I

Award year

2020

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
MAINSTREAM ENGINEERING CORP
Proposal award date
2020-08-12
Contract end date
2021-03-01
UEI
YR8FJBGXWRR1
Solicitation number
SBIR_20_P1
Topic code
Z2

Research abstract

Mainstream proposes a Modular Membrane Controlled Three-phase Deployable Radiator (MMC-TDR) that has a turndown ratio of 200:1, a mass of only 7.8 kg, and design life of over 15 years. The key enabling components of the MMC-TDR are 1) a passive, reliable membrane phase separator for robust two-phase flow control in the absence of gravity, 2) a passive bypass valve which regulates flowrates in the radiator to control heat rejection, and 3) a modular, deployable tube-on-plate three phase radiator design which is three-phase compatible. The system integrates with a two-phase pumped loop using ammonia as the process fluid. The MMC-TDR uses an integrated membrane phase separator that achieves separation via capillary action, so that operation is insensitive to gravity and inertia effects. Separate vapor and liquid ammonia streams are distributed to the freezable radiator through two distributions headers. The subcooled liquid from both streams is combined at the outlet of the radiator array in the collection header. The MMC-TDR will use increased pressure losses and heat transfer from longer channel lengths with a variable opening PCM bypass valve to selectively reduce flow through outer most channels as heat load is reduced. The reduction in flow will results in high degrees of subcooling until freezing occurs. The percentage of flow through the bypass line vs. the radiator channels is passively controlled by modulating the bypass valve position, increasing or reducing the bypass line pressure drop relative to the channel pressure drops. The PCM bypass valve regulates the flow through the system to achieve the desired subcooled temperature, effectively allowing the radiator channels to gradually lose flow and freeze during periods of low desired heat dissipation. The freezable radiator panel is constructed of a series of parallel ldquo;Urdquo; channels. The channels are constructed of aluminum encased Inconel tubes.

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

518 SBIR/STTR records share this UEI (1987–2025). Reported award amounts total $184,860,329. Reported amounts are not federal obligations.

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

Agencies: Department of Defense, Department of Energy, National Aeronautics and Space Administration, Department of Transportation, Department of Health and Human Services, Environmental Protection Agency

Agency intelligence

National Aeronautics and Space Administration

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