
Overview
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.
The unit comes in multiple configurations ensuring compliance to common satellite propellants, fluidics and avionics interfaces.
PERFORMANCE:
- Pressure range (MEOP): 0 ... 10 bar, 30 bar, 100 bar, 200 bar, 320 bar
- Proof pressure: 1.5 x MEOP
- Burst pressure: 4 x MEOP
- Accuracy: ±0.25% FS
- Temperature sensing: internal and/or external thermistor
INTERFACE:
- Supply voltage: 8 V - 34 VDC
- Current consumption: < 10 mA
- Output interface: 0 V - 5 V (analog)
- Mechanical interface: 2 x M3 fasteners
- Size: 62 mm x 36 mm x 36 mm
- Mass: starting from 110g
ENVIRONMENTAL:
Temperature range (operational): -30 °C to +60 °C operational
Temperature range (non-operational): -40 °C to +70 °C operational
Radiation: TID > 30 krad, SEL immune
Random vibration: 14.1 grms
Shock: SRS 1000g (ECSS-E-ST-10-03C)
Compatibility: MON, MMH, ADN, HAN, HTP, N2O, Water, He, N2, Xe, Kr, Ar
Properties
Overview
- Name
- Garnet Pressure Transducer
- Supplier
- Ascend Beyond Space
- Type
- Pressure & Flow Sensor
- Flight proven
- No
Details
- Dry Mass
- 0.11 kg
Delivery and customization
- Lead time
- 2 to 6 months
- Customization / NRE
Unknown