Propulsion Control Components Products:
Spacecraft Components
Single Stage Regulator (Gas)
Type: Single Stage, Gas
Note: All of our products are flexible and customizable to meet your specific needs. Please contact us for more information.
Typical Perfomance Specifications
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Fluid
GN2, GHe
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Inlet Max Pressures
290 to 50 psig (20.0 to 3.4 bar)
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Inlet Proof Pressures
464 psig (32.0 bar)
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Inlet Burst Pressures
754 psig (52.0 bar)
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Outlet Regulated Pressures
5 psig (0.34 bar)
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Outlet Proof Pressures
290 psig (20.0 bar)
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Outlet Burst Pressures
507 psig (35 bar)
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Max Lockup Pressures
7 psig (0.48 bar)
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Flow Capability
0.07 SCFM (2 slpm)
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Internal Leakage
0.01 scc/min GN2 maximum
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External Leakage
< 1x10-5 scc/min GN2
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Cycle Life
1,000 max
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Weight
0.66 lb (0.30 kg)
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Inlet Filtration
60 micron absolute
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Thermal Operating Capability
-4°F to +158°F (-20°C to +70°C)
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Wetted Materials
Stainless Steel or Vespel®
Most of the listed performance parameters reflect the program requirements and not the design limitations of the valve. In general most valves will perform better than listed in the following areas: system pressure, flow rate, pressure drop, internal leakage and response time.
Related Products
Related Market Information
Contact Us
Bill Vogt
Spacecraft Fluid Controls Sales Manager
+1-716-687-4109
- Propulsion Controls
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- Spacecraft Fluids
- Components
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- Solenoid Actuated
- Torque Motor Actuated, Mono-propellant
- Torque Motor Actuated, Bi-Propellant
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- Regulators
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- Solenoid Actuated
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- Solenoid Actuated, Dual Seat
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- Throttle Valve
- Cold Gas Thrusters
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- Fuel Oxidizer Manifold
- Helium Manifold
- High Purity Gas Management Assembly
- Reaction Control System
- Xenon Flow Controller
- Xenon Feed System
- Components
- Tactical Missiles
