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A Reduced gravity Chilldown and Transfer Investigation using Cryogens (ARCTIC)
Canceled
TRL 6 (started at 4, targeting 6)
Description
The Reduced Gravity Cryogenic Transfer Project will investigate three chilldown and two liquid injection methods for chilling and filling cryogenic tanks in a low-gravity environment. Researchers also plan to collect data on flow visualization, pressure, temperature, and flow produced during cryogenic propellant transfers. Information gathered during these parabolic flights could provide the data and operational experience necessary to advance in-space cryogenic transfer processes.
Benefits
Microgravity cryogenic transfers enable Lunar or Martian ascent or descent stages, upper stages, and aggregation/depots Efficient cryogenic fluid transfer methods will reduce the amount of propellant consumed or time needed for chilldown of tanks LN2 tank chilldown tests performed onboard parabolic flights will yield data and operational experience in microgravity environment to mature in-space cryogenic transfer
Details
| Technology area | Propulsion Systems > Chemical Space Propulsion > Integrated Systems and Ancillary Technologies |
| Program | Flight Opportunities (FO) |
| Lead organization | Glenn Research Center, Cleveland, OH |
| Start date | 2021-08-01 |
| End date | 2022-07-31 |
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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