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A CubeSat-Scale Testbed for Cryogenic Fluid Management Technologies

Completed TRL 7 (started at 6, targeting 7)

Description

NASA has identified in-space cryogenic fluid management (CFM) as a high priority for technology development because the construction of an in-space propellant infrastructure is anticipated to dramatically decrease costs across a broad spectrum of missions. This importance is reflected in the designation of CFM as a Flagship Technology Demonstration Mission (FTD-2) as well as a mission at the level of Crosscutting Technologies (CRYOTE). Sierra Lobo proposes to develop a CFM testbed at the scale of an Edison Demonstration Mission (CryoCube) that would serve as a platform for a series of flight tests of many major CFM technologies. The missions will be designed to be conducted as stand-alone satellites, without reliance on propellant transfer from an upper stage, in order to provide the greatest possible flexibility for launch vehicle selection. Follow-up missions using dedicated small satellite launch vehicles could take advantage of the technology demonstrated during this SBIR program, and could be performed as funding becomes available instead of depending on the allocation in a large block.

Benefits

Sierra Lobo will endeavor to transfer technologies developed during the course of the project into other small satellite applications. The thermal management technology to be developed is directly applicable to satellites that require sensor cooling. The technology could also contribute to propellant storage and transfer to extend the life of small satellites; for example, through enabling the storage of xenon in a liquid state.

Although a large number of CFM technologies have been matured by ground testing, many key technologies await flight testing. CubeSat-scale tests can improve the understanding of the phenomena affecting many of the technologies; for example, liquid acquisition and zero boil-off storage. Some of the technologies can be tested as they would be used in a full-scale depot; for example, pressure and acceleration sensors, and the sensors used in the Reduced Gravity Cryo-TrackerREG mass gauging system.

Details

Technology areaPropulsion Systems > Chemical Space Propulsion > Cryogenic Propulsion
ProgramSmall Business Innovation Research/Small Business Tech Transfer (SBIR/STTR)
Lead organizationSierra Lobo, Inc., Fremont, OH
Start date2011-02-18
End date2011-09-29

Project contacts

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How to get involved

This is a mature technology (TRL 7) — the realistic path in is usually NASA's Technology Transfer Program: licensing an existing NASA patent, or a Space Act Agreement to use NASA facilities/expertise directly. NASA also runs a startup licensing program with no upfront fee for companies formed to commercialize a specific NASA technology.

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