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Stability of in-space cryogenic systems

Completed TRL 6 (started at 4, targeting 6)

Description

The Stability of In-Space Cryogenic Systems experiment will study the stability of spacecraft propellant during refueling as it relates to temperature and mechanical disturbances,which are important measurements for preventing flow control failure and equipment damage. Testing on parabolic flights will assess the threshold of heat pulses and vibration at which flow oscillations are triggered. Tests will also evaluate the factors controlling liquid nitrogen flow stability and, if successful, result in a strategy to enhance propellant stability and prevent hydraulic shocks. 

Problem Statement 
The storage and transfer of cryogenic propellants in microgravity is critical for lunar and deep space exploration. Thermal-hydrodynamic instabilities on long-duration missions could make controlling propellant and the propellant transfer process more difficult. More research is needed to determine safety parameters for propellant refueling with heat and mechanical disturbances.

Technology Maturation 
Knowledge gained from parabolic flight tests will advance technology for cryogenic transport operations in space–to which NASA has currently assigned a TRL of 4 –to TRL 6. This demonstration will assess the role of gravity in propellant transport by measuring the contrast in heat and mechanical disturbances between a ground and microgravity environment, supporting the development of propellant stability guidelines.


Summary of Flight Test
2023-05-08, 2023-11-28, & 2024-02-26 Collaborative work of the New Jersey Institute of Technology and Princeton CryoTech teams developed a successful flow system to transport a cryogenic fluid in a low-gravity environment without pumps and high pressure gas cylinders. Results acquired in parabolic flight tests provide critical information for the design of a flow system for refueling of cryogenic propellants in space.

Benefits

This knowledge payload could advance the field of cryogenic storage and transfer overall. In addressing this critical NASA need, this technology will establish guidelines for and reduce the risk of in-space propellant transfer by analyzing the role of gravity in potential propellant disturbances. These guidelines are crucial for sustainable, long-duration space missions as well as ground-based cryogenic management. This would benefit NASA missions and the commercial space industry.

Future Customers
•Long-duration space exploration missions
•Ground-based cryogenic applications

Details

Technology areaPropulsion Systems > Chemical Space Propulsion > Cryogenic Propulsion
ProgramFlight Opportunities (FO)
Lead organizationNew Jersey Institute of Technology, Newark, NJ
Start date2021-01-01
End date2026-01-31

Project contacts

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How to get involved

This is early/mid-stage (TRL 6) — 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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