Satellite Propulsion Regulator Specifications HomeSpace Propulsion SystemsSatellite Propulsion Reg... Specifications Item Imperial Metric Medium Helium Inlet Pressure 400 to 4,000 psig (28 to 276 barg) Outlet Pressure 232 psig (16 barg) Lockup Pressure 247 psig (17 barg) Proof Pressure 6,000 psig (414 barg) Burst Pressure 12,000 psig (827 barg) Flow 6.7 scfm Internal Leakage 5.6 x 10-2 sccs External Leakage 1.0 x 10-6 sccs Weight 2.15 lb max (0.98 kg) Operating Environment Item Imperial Metric Temperature -50 to 120 deg F (-46 to 49 deg C) Humidity 0 to 95% Vibration 12.1 grms each axis Home Capabilities Customers Suppliers Careers News About Satellite Propulsion Regulator Product Contacts USA Cobham Mission Systems, Orchard Park, USA 10 Cobham Drive, Orchard Park, New York, USA 14127. Tel +1 716 662 0006 Fax +1 716 662 0747 Cobham Mission Systems Orchard Park Inc. View location Contact office
Item Imperial Metric Medium Helium Inlet Pressure 400 to 4,000 psig (28 to 276 barg) Outlet Pressure 232 psig (16 barg) Lockup Pressure 247 psig (17 barg) Proof Pressure 6,000 psig (414 barg) Burst Pressure 12,000 psig (827 barg) Flow 6.7 scfm Internal Leakage 5.6 x 10-2 sccs External Leakage 1.0 x 10-6 sccs Weight 2.15 lb max (0.98 kg) Operating Environment Item Imperial Metric Temperature -50 to 120 deg F (-46 to 49 deg C) Humidity 0 to 95% Vibration 12.1 grms each axis