GARNET PRESSURE AND TEMPERATURE SENSOR
The easiest way to monitor your propulsion systems
The Garnet propellant measurement unit combines pressure and temperature sensing as well as the signal conditioning electronics.
Designed as a seamless plug-and-play subsystem, it serves the critical function of assessing propellant levels from tank pressure and temperature throughout the lifecycle and particularly at end-of-life stages.
In addition to the multiple customization options, the unit comes in two main variants: analog output (Garnet-A) and digital output (Garnet-D).
USE CASE EXAMPLE
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Multiple sensors, tracking the different pressure stages, tank and valve temperatures.
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Single unregulated power bus compatible
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Single digital communication bus minimizing use of OBC interfaces count.
Performance
Pressure range (MEOP)
Proof pressure
Burst pressure
Accuracy
Temperature sensing
0 ... 10 bar, 30 bar, 100 bar, 200 bar, 320 bar
1.5 x MEOP
4 x MEOP
±0.25% FS at BOL
±0.4% FS at EOL (pending mission profile)
Internal thermistor (1 kΩ @ 25°C PTC)
Interface
Electrical interface
Supply voltage
Current consumption
Output interface
Mechanical interface
Size
Mass
Wetted material
Fluidic interface
9-pin Nano-D-Sub (MIL-DTL-32139)
8 V - 34 VDC
< 10 mA
0 V - 5 V (analog)
2 x M3 fasteners
62 mm x 36 mm x 36 mm
Starting from 110 g
AISI 316L
1/4" weldable tube
Environmental
Temperature range
Radiation
Random vibration
Shock
Compatibility
-30 °C to +60 °C operational
-40 °C to +70 °C non-operational
TID > 30 krad, SEL immune
14.1 grms
SRS 1000 g (ECSS-E-ST-10-03C)
MON, MMH, ADN, HAN, HTP, N2O, Water, He, N2, Xe, Kr, Ar
Customizations
Electrical interfaces
Fluidics interface
Wetted material
Pressure range
Output interfaces
Analysis
Flying leads, custom connector
VCR, Swagelok tube fitting
Ti-6Al-4V, Hastelloy C-276
Custom range and temperature calibration
0 V - 3 V (analog)
PSA, WCA, FIT, Structural