Our products are modular and built on flight-proven architectures. Each can be tailored to your mission: orbit, radiation environment, interface set and budget.
Flight computers
One hardware baseline for every orbit
GEOPARS and LEOPARS share one modular architecture: a common backplane and PCB layout that takes either radiation-hardened or radiation-tolerant components. Moving from LEO to GEO or low lunar orbit means changing modules, not redesigning the computer.
High-reliability OBC for GEO and long-life missions
GEOPARS Satellite Flight Computer
In design
- Radiation-hardened and/or radiation-tolerant components
- Multi-core LEON processor with SoC system controller
- DDR RAM and MRAM boot memory
- 4 × SpaceWire, 2 × MIL-STD-1553B (internally redundant), 4 × CAN, 4 × UART
- 2 × CCSDS-compliant TM/TC interfaces; 28 V power
- 100 × 200 mm or SpaceVPX form factor
- Optional discrete-interface modules: HPC, BSM, BDM, ASM, TSM
Cost-optimised OBC for LEO and small satellites
LEOPARS Satellite Flight Computer
In design
- COTS, radiation-tolerant and space-proven components combined
- Multi-core processor with SoC system controller
- DDR RAM, MRAM boot memory, NAND Flash data storage
- 4 × SpaceWire, 2 × MIL-STD-1553B, 4 × CAN, 4 × UART
- 2 × CCSDS TM/TC interfaces; 28 V power
- 100 × 200 mm or SpaceVPX form factor
In development · 2026–2028
Neuro-Orbit AI-Enabled Flight Computer
Our next-generation flight computer pairs a radiation-tolerant FPGA SoC, which runs the critical flight software, with a dedicated AI accelerator. It runs anomaly detection, AI star tracking, GNSS navigation and on-board image processing in orbit. It can replace separate OBC, star tracker processor, GNSS receiver and payload computer boxes with a single unit.
Neuro-Orbit is supported by the TÜBİTAK-TEYDEB 1501 Industrial R&D Projects Support Programme (Project No: 3261148).
Navigation
Precise orbit and time determination for LEO, MEO and GEO
TetraGNSS Multi-Band Space GNSS Receiver
In development (FPGA IP core in test)
- GPS, Galileo, GLONASS and BeiDou
- L1, L5, E1, E5 and E6 bands
- Software-defined architecture on an integrated processor + FPGA/SoC
- 2 × CAN, 2 × UART, optional 2 × MIL-STD-1553B
- PVT and 1PPS outputs; 28 V power
- Can be adapted to new navigation signals
Sub-metre positioning for air, land, sea and orbit
TetraNav-S Precision GNSS Receiver
In development
- GPS (L1, L2, L5) + Galileo (E1, E5, E6)
- 0.2–0.5 m accuracy with Galileo High Accuracy Service, with no ground station or subscription
- < 0.5 kg (mission config.) / 2 kg (full feature), < 15 W
- –30 °C to +60 °C
- MIL-STD-1553B / RS-422 / CAN; nominal, redundant and test 1PPS
Terrain-relative navigation for lunar landing and orbit
LuNav Vision-Based Navigation
In development
- Dual-camera support; adaptable to different optics
- Unified processor + FPGA architecture for real-time feature matching
- Visual simulation support and detector calibration
- 2 × MIL-STD-1553B, 2 × CAN, 2 × SpaceWire, 2 × SERDES/MGT, 2 × UART
- 28 V power interface
Building blocks
Spacecraft modules
Build flight units from proven building blocks. Every module shares the same mechanical and electrical conventions, so a new mission gets a tailored unit quickly and at low cost.
Test & verification
Test equipment
- MIL-STD-1553B test equipment
- Dual-channel CAN test equipment
- CCSDS-compliant S-band emulator
- Processor / FPGA debugging equipment
- Time-synchronisation test equipment
- 8/16-channel RS-422/485/232 signal monitoring and recording
- 4/8-channel RS-422/485/232 communication test equipment
- 2-channel analog measurement, monitoring and recording
- 8-channel 24-bit 200 ksps analog recorder (load cell / strain gauge)
Have a mission in mind?
Share your platform, orbit and interface needs, and let’s find the right solution together, engineer to engineer.