Tavis satellite transducers have provided propulsion measurements for journeys to orbit other planets, while other Tavis instruments have actually landed on planetary surfaces or measured pressures as the spacecraft plummets through other solar system atmospheres.









Previous hardware for missions to Mars, Jupiter, Venus and the Moon have featured one or more of the following:
  • Very low barometric pressure measurements with high proof
  • Severe thermal environments
  • Tether cable for thermal separation between gage and electronics
  • Low power consumption
  • Long-term stability over thermal environments
  • Ice, sand, dust immunity
  • High-cycle power on-off
  • Spores bake-out
  • Zero Outgassing
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Sample Product

Pressure Range

Weight

Input Voltage

Power

Compensated Temps

Vibration

Quantity
N/A 0 - 0.174 psia 0 - 15 psia N/A 454 gm Max N/A 24 - 36 VDC N/A 10 mA Max N/A -50 ºC to +50 ºC (Operating -65 ºF to +200 ºF) N/A
N/A 0 - 2.5 psid to 0 - 5 psid N/A 14 oz Max N/A 25 - 30 VDC N/A 7 mA Nominal N/A -65 ºF to +165 ºF N/A 57 grms
N/A 0 - 5 psia N/A 13 oz Max N/A 24 - 32 VDC N/A 10 mA Max N/A -54 ºC to +93 ºC (Gage Operating -155 ºC to +125 ºC) N/A 23.5 grms
N/A 0 - 0.01 psid to 0 - 11 psid N/A 3.5 lb Max N/A 20 - 40 VDC N/A 10 mA Max N/A -65 ºF to +165 ºF (Operating -65 ºF to 200 ºF) N/A 20 g pk
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