The Air Force Rocket Lab Afrl At Edwards Afb Requires Modest Pressure Modest Flow Cryogenic Ball Valves For Use In The Multiscale Rocket Engine Test Mret Facility Mret Is A New High Pressure Small Scale Rocket Engine Test Facility That Is Being Constructed In Addition To 10 000Psi Flow Systems This Facility Has Several Lower Pressure Flow Systems Needed To Maintain Cryogenic Temperatures These Valves Are Needed For Those Temperature Maintenance Systems Please Review The Attached Combined Synopsis Solicitation For The Cryo Ball Valve Specifications
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