Pressure Sensor
Thin-film strain-gauge pressure sensor for rocket/space systems (0–60 MPa range, 0.25% error, 0.15 kg, -196 to +50 °C, high vibration/shock resistance).
Technical specifications
- Purpose
- Static-dynamic pressure measurement for rocket and space technology information-measuring systems
- Estimated production/delivery time
- 6 months
- Customization
- Can be adapted to customer requirements
- Measurement ranges, MPa
- 0–1; 0–1.5; 0–2; 0–3; 0–4; 0–6; 0–8; 0–10; 0–15; 0–25; 0–40; 0–60
- Basic error, % of measuring range
- ≤0.25
- Supply voltage, V
- 5–14
- Medium temperature, °C
- -196 to +50 (briefly up to 2700 with transition tube)
- Mass, kg
- 0.15
- Features
- High precision; high metrological stability under vibration, shock, and external factors
- Design
- Thin-film strain gauge monoblock with cable jumper
- TRL
- 9
About
The Pressure Sensor is a thin-film strain-gauge absolute pressure sensor designed as part of information-measuring systems for rocket and space technology. It measures static-dynamic pressure of liquid and gaseous media. Measurement ranges: 0–1, 0–1.5, 0–2, 0–3, 0–4, 0–6, 0–8, 0–10, 0–15, 0–25, 0–40, 0–60 MPa. Basic error ≤0.25% of measuring range. Supply voltage 5–14 V, medium temperature -196 to +50 °C (briefly up to 2700 °C with a transition tube). Mass 0.15 kg. Features high precision and high metrological stability under vibration, shock, and other external factors. Monoblock design with cable jumper. Delivery 6 months. Customizable.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
