Aerospace Prototype Pressure Vessel for Fuel Storage at Cryogenic Temperatures:

Performance characteristics; end service life; "cryo-treatment" stress/strain relaxation; degradation of constituent fiber and resins, etc., are just some of the many parameters and features being evaluated under contracts with NASA to improve the design of "Deep Space Probes" and their resulting reliability and efficiency.


Read the Cryogenics Phase 1 Final Report to NASA


Carbon Fiber and Zylon Filament Wound Cylinders