Propulsion Control Components Products:
Spacecraft Components
High Flow Pressure Regulator
Specifications
-
Fluid
GHe
-
Inlet Maximum Pressure
5000 psig (345 bar)
-
Inlet Proof Pressure
7500 psig (517 bar)
-
Inlet Burst Pressure
12,500 psig (862 bar)
-
Outlet Regulated Set Point Pressure
Between 400 and 800 psig (27.6 and 55 bar)
-
Maximum Lockup Pressure
Nominal Setpoint +40 psi
-
Outlet Proof Pressure
1200 psig
-
Outlet Burst Pressure
2000 psig
-
Flow Capability
Zero to 0.2 lb/sec at 70 degree F, 700 psig setpoint
-
Internal Leakage
Bubble Tight
-
External Leakage
< 1x10-6 sccs GHe
-
Cycle Life
> 10,000 Lockup-Full Flow-Lockup
-
Flight Weight
3.3 lb (1.5Kg)
Related Products
Related Market Information
Contact Us
Bill Vogt
Spacecraft Fluid Controls Sales Manager
+1-716-687-4109
- Propulsion Controls
-
- Spacecraft Fluids
- Components
-
- Solenoid Actuated
- Torque Motor Actuated, Mono-propellant
- Torque Motor Actuated, Bi-Propellant
- Linear Force Motor Actuated
- Fill & Drain Valves
- Regulators
-
- Solenoid Actuated
- Solenoid Actuated, Single Seat
- Solenoid Actuated, Dual Seat
- Torque Motor Actuated
- Throttle Valve
- Cold Gas Thrusters
-
-
- Fuel Oxidizer Manifold
- Helium Manifold
- High Purity Gas Management Assembly
- Reaction Control System
- Xenon Flow Controller
- Xenon Feed System
- Components
- Tactical Missiles
-
Space and Defense Events
Singapore Airshow
Learn More
February 14-19
National Space Symposium
April 16-19 -
Related Products
-
Learn More About Our Recent Acquisitions
-
Connect with Moog
