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Liquid-fuel Rocket Engine

Pressure Sensor Vt 212

  • Purpose: Measurement of the static-dynamic pressure of liquid and gaseous aggressive and non-aggressive media in control systems and diagnostics of liquid rocket engines. Works with the converter Vt 5509 or Vt 5510, Vt 5514.
  • Estimated production / delivery time (months): 6
  • Flight qualification of the product: Yes
  • Possibility to adapt the product to customer requirements: Yes
ParameterValue
Range of measurements, Mpa0-2,8; 0-4; 0-5,6; 0-8; 0-11; 0-16; 0-22; 0-30; 0-45; 0-60; 0-90; 0-125
The basic reduced error, %0,6
Nominal output signal Un, mV9
Supply voltage6±1,2
Weight, kg, not more0,12

Features:

  • high stability of metrological characteristics during operation in a wide temperature range, the effects of vibration, shock and other external factors;
  • manufactured according to the "Regulation 98".

Version: strain gauge sensor with cable jumper. At the request of the customer (in the absence of temperature control of the sensor on the product) it is manufactured with a heat-receiving sleeve. The type of explosion protection of the sensor is “Tight sheath”, cable jumper - “Intact cable network”.