CDH-FS
CAVU Aerospace
Main OBC for SmallSat platform
Technical specifications
- Memory (RAM)
- 160Mbits MRAM 40 bits width (128Mbits+32Mbits ECC)
- Memory (ROM)
- 96Mbits MRAM (Configurable as Triple 32Mbits)
- Memory (Nonvolatile Flash)
- Total 24Gbit SLC NAND Flash (Triple 8G), 256K Serial FRAM, 256M Serial NOR
- Radiation hardness (Total Ionizing Dose)
- 30Krad (Si)/yr
- Operating temperature
- -40 C to +85 C
- Pressure
- 10 bar
- Shocks
- 2000 g, 2000-10000 Hz
- Random vibrations
- 14 g(RMS) 3-Axis , 20~2000 Hz
- Expected lifetime
- 3-5 years in LEO
- Dimensions
- 205x203x87 mm
- Mass
- 4250gr
- Supply voltage
- 5 V ±5%
- Power consumption
- 3 W ~ 5 W
- Interfaces (Digital Outputs)
- 100 (5 V/3.3 V)
- Interfaces (Analog To Digital Converter)
- 128 (16bits, -10V~+10 V)
About
The CAVU CDH-FS represents the pinnacle of on-board computer systems, featuring a fully redundant FPGA-based architecture designed to guarantee continuous operation. With a backup processor that seamlessly engages upon primary processor failure, this system is not just reliable; it’s essential for critical missions. Engineered to resist severe space conditions like radiation and cosmic rays, it leverages the efficiency and SEU immunity of Microchip/Microsemi SmartFusion2 and ProASIC3 Flash-based FPGAs.
Documentation
Need the full ICD, test reports or a specific revision? Ask the supplier directly.