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Passive Reduction of Orbital debris and Thermal Evaporation for Cryogenic Tanks (PROTECTor)

Active TRL 3 (started at 3, targeting 6)

Description

This activity's objective is to develop a combined protection systems that combines thermal protection (i.e. MLI) and hypervelocity impact protection. Testing will include hypervelocity impact testing at both the coupon and tank applied level as well as thermal calorimeter testing, liquid hydrogen tank applied testing, and tank applied vibration testing.

Benefits

Combining these protection systems on cryogenic tanks will decrease their thickness and allow for a significant volumetric increase for tanks as well as a reduction in mass.

Details

Technology areaThermal Management Systems > Cryogenic Systems > In-Space Propellant Storage and Use
ProgramTechnology Demonstration Missions (TDM)
Lead organizationGlenn Research Center, Cleveland, OH
Start date2025-06-01
End date2029-11-30

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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