Pressure Transducers for Satellite Propulsion
All Categories
Inconel 718 and 304L CRES materials are used in our satellite transducers because of their compatibility with caustic propulsion media such as MMH, NOX, MON-3, etc. Most satellite transducer designs manufactured by Tavis utilize a ¼-inch tube stub for orbital tube welding into the spacecraft manifold tubing. The tube stubs are typically seamless 304L or 321; however, some designs incorporate a Titanium-to-304L transition tube for use with Titanium spacecraft plumbing.
Existing designs provide capabilities such as:
Existing designs provide capabilities such as:
- High pyro shock tolerance for nearby valves and separation nuts
- Inherent secondary barrier for burst pressure containment
- High proof and burst pressure capability
- Connector or pigtail configurations
- EMI filtering and immunity
- Compact size
- Low power consumption for long orbit life requirements
- Space-grade parts; radiation-hardened components and shielding
- No mounting feet option, or one-piece case and mounting feet configurations
- Soldering procedures based on NASA-STD-8739.3
Sample Product |
Pressure Range |
Input Voltage |
Output Signal |
Vibration |
Quantity |
---|---|---|---|---|---|
10496 10496/Asset/PN-10496.JPG | Pressure Range N/A 30 psia to 5000 psia | Input Voltage N/A 22 - 38 VDC | Output Signal N/A 0.0 - 5.0 VDC0.5 - 5.5 VDC | Vibration N/A 36.9 grms | |
10430 10430/Asset/PN-10430.JPG | Pressure Range N/A 0-200 psia | Input Voltage N/A 24 - 33 VDC | Output Signal N/A 0.0 - 5.0 VDC | Vibration N/A 19.3 grms | |
10499 10499/Asset/PN-10499.JPG | Pressure Range N/A 0 to 550 psia 50 to 400 psia | Input Voltage N/A 22 - 36 VDC | Output Signal N/A 0.5 - 6.0 VDC | Vibration N/A 13.92 grms | |
30000 30000/Asset/PN-30000.JPG | Pressure Range N/A 30 psia to 6000 psia | Input Voltage N/A 24 - 32 VDC | Output Signal N/A 0.0 - 5.0 VDC | Vibration N/A 15 grms |