Model 2211
Output : 3mV/V or 2mV/V (nominal excitation of 10VDC)
Pressure Range : 15~20,000 psi
Temperature Range : -450℉~+400℉
Static Accuracy : 0.25% (standard)
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Coolant Systems (cryogenic)
Liquid Oxygen (LOX)
Rocket Engine Testing
Research Laboratories
Hydrogen & Hypergolic |
Propulsion Systems (cryogenic)
Launch Pad Gases (cryogenic)
High Temperature
Laser Systems R&D
Launch Vehicles |
High Speed Response
Auxiliary Power Units (APU)
Jet Engine Test Stands
Aircraft Systems Test Stands |
Model 2911
Output : 0~5VDC (non regulated 22~36VDC)
Pressure Range : 2~20,000 psi
Temperature Range : -65℉~+250℉
Static Accuracy : 0.25% (standard)
option : EMI Protection
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Coolant Systems
Launch Pad Materials
National Research Labs
Special EMI Protection
Aircraft Cabin O2
Target Missiles
Unmanned Aircraft |
Propulsion Systems
Rocket Engine Test Stands
Laser Systems R&D
Barometric
OBOG Systems
Launch Vehicles
Hypersonic Aircraft |
Aircraft Systems Test Stands
Jet Engine Test Stands
Hydrogen & Hypergolic
Hydraulic Systems
Sounding Rockets
High Cyclic Rate Test Stand
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모델명
