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A Reliable, Efficient Cryogenic Propellant Mixing Pump with No Moving Parts
Completed
TRL 3 (started at 2, targeting 3)
Description
Refueling spacecraft in space offers tremendous benefits for increased spacecraft payload capacity and reduced launch cost. A key technology challenge for space refueling is the storage of liquid cryogenic fuel in space. To meet this need, we propose to develop a reliable, compact, efficient cryogenic mixing pump with no moving parts. The mixing pump will prevent thermal stratification of the cryogen and simplify pressure control for storage tanks. The mixing pump uses an innovative thermodynamic process to generate fluid jets to promote fluid mixing, eliminating the need for mechanical pumps. Our innovative mechanism will be able to self-prime and generate a high-pressure rise. The device will significantly enhance the reliability of pressure control systems for storage tanks. In Phase I, we will prove the feasibility of our approach through building and testing a proof-of-concept mixing pump and developing an analytical model to optimize the mixing pump design. In Phase II, we will build and test a laboratory-scale cryogenic mixing pump and demonstrate its performance in a representative cryogenic environment.
Benefits
The technology developed in this project will enable reliable long-term and short-term cryogenic propellant storage in space for refueling. The mixing pump will enable effective pressure control for cryogenic tanks by maintaining a fluid uniform temperature. Its high reliability will significantly enhance the effectiveness of the pressure control mechanism. The device developed in this project can also be used as a two-phase cryogenic pump with no impellers or pistons to enable reliable cryogen transfer for space applications.
The technology developed in this project has applications in reliable two-phase pumps for cryogenic fluids and refrigerant flows. Applications include cryogenic two-phase cooling systems for superconductors. The technology also has applications in thermal management systems for advanced electronics and photonics systems, as well as advanced environmental control systems for future military vehicles.
Details
| Technology area | Thermal Management Systems > Cryogenic Systems > In-Space Propellant Storage and Use |
| Program | Small Business Innovation Research/Small Business Tech Transfer (SBIR/STTR) |
| Lead organization | Creare, LLC, Hanover, NH |
| Start date | 2013-05-23 |
| End date | 2013-11-23 |
Project contacts
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How to get involved
This is early/mid-stage (TRL 3) — the most realistic path in is NASA SBIR/STTR, which funds small businesses and research institutions to develop technology aligned with NASA's needs (equity-free, phased funding). Check whether a current SBIR/STTR solicitation topic overlaps with this project's technology area, or contact the project directly (above) to ask.
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