Spacecraft Avionics
Moog's Advanced Avionics Systems are designed specifically for spacecraft & payload applications. Systems are available for integrated Command and Data Handling (C&DH), Electrical Power System (EPS) and payload applications. Design options include single string and redundant systems. All avionics are tailored to meet the mission requirements. Existing designs are drawn on where advantageous and new designs are created where significant benefits may result.听Product and capabilities include high-TRL demonstrated heritage and high-performance next-generation designs. 刘玥首次大战黑人 are designed for performance and radiation capability in all earth orbits and beyond.
Next Generation Processors and Memory
Looking to the future of on-orbit space computing applications, we offer high-performance, next-generation products for Processors (GPU, DSP and ARM) as well as Memory (NAND FLASH and DDR4). These state-of-the-art technologies are radiation-tested and can be provided in component, board-level or integrated assembly. These products are a direct result of our continued investment into future space technologies and represent orders-of-magnitude performance improvement over traditional space-qualified comparable components.
DOCUMENT DOWNLOADS:
- Single Board Computer - Low Power GPU
- Single Board Computer - Multi-Core DSP/ARM
- Single Board Computer - MultiCore ARM
- Single Board Computer - GPU
- Flash Memory Board - 10Tb
- Radiation Tolerant Solid State Recorder
- Radiation Tested Components
听
Spacecraft Avionics
Moog鈥檚 Integrated Avionics Unit (IAU) and Main Avionics Controller (MAC) provide C&DH/EPS solutions for a full range of spacecraft needs. From the cost-optimized MAC to the fully-redundant configuration IAU when failure is not an option, 刘玥首次大战黑人provides spacecraft controls options for every mission.
MAC & IAU: Avionics For Any Mission
| 听 | FEATURE | SIZE (cm) | MASS (kg) | POWER (W) | MAX POWER THRUPUT (W) | EEE PARTS | ORBIT | MISSION LIFE | ENVIRONMENT | FORM FACTOR | CAPACITY | REDUNDANCY APPROACH |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
 |
MAC | 23.6 x 24.5 x 8.8 | 5.8 (TYP) | 12-40 | 2,100 | Screened Automotive | LEO | 3-5 Years (TYP) | GEVS | SLICE | Variable | Optional Integrated Redundancy with Dual-Box Configuration |
|
MAC-HR | 23.6 x 24.5 x 8.8 | 5.8 (TYP) | 12-40 | 3,000 | EEE-INST-002 LEVEL 1/2/3 | LEO 鈥� GEO INTERPLANETARY | 3-10 Years (TYP) | GEVS | SLICE | Variable | Optional Integrated Redundancy with Dual-Box Configuration |
 |
Redundant MAC (Integrated Redundancy) |
23.6 x 24.5 x 8.8 X 2 |
5.8 (TYP) X 2 | 15-80 | 3,000 | SCREENED AUTOMOTIVE; EEE-INST-002 LEVEL 1/2/3 | LEO 鈥� GEO INTERPLANETARY | 5-15 (TYP) | GEVS | SLICE | Variable | Integrated Redundancy State Data Storage Dead Bus Recovery |
 |
IAU Level 3 | 25.1 x 21 x 11.9 | 8.3 (TYP) | 37 | 1,800 | EEE-INST-002 LEVEL 3 | LEO | 3-5 Years (TYP) | GEVS | 3U cPCI | 10 SLOTS | Optional Integrated Redundancy with Dual-Box Configuration |
|
IAU Level 2 | 25.1 x 21 x 11.9 | 8.3 (TYP) | 37 | 1,800 | EEE-INST-002 LEVEL 2 | LEO 鈥� GEO INTERPLANETARY | 5-7 Years (TYP) | GEVS | 3U cPCI | 10 SLOTS | Optional Integrated Redundancy with Dual-Box Configuration |
|
IAU Level 1 | 25.1 x 21 x 11.9 | 8.3 (TYP) | 37 | 1,800 | EEE-INST-002 LEVEL 1 | LEO 鈥� GEO INTERPLANETARY | 7-10 Years (TYP) | GEVS | 3U cPCI | 10 SLOTS | Optional Integrated Redundancy with Dual-Box Configuration |
 |
Redundant IAU (Integrated Redundancy) |
25.1 x 21 x 11.9 x2 | 8.3 (TYP) x 2 | 42 (Warm Spare) 65 (Hot Spare) | 1,800 | EEE-INST-002 LEVEL 1/2/3 | LEO 鈥� GEO INTERPLANETARY | 10 - 15 Years (TYP) | GEVS | 3U cPCI | 10 SLOTS PER IAU | Integrated Redundancy State Data Storage Dead Bus Recovery |
 |
Redundant IAU (With Redundant Management Unit) |
IAU 25.1 x 21 x 11.9 x2 RMU 12.2 x 10.4 x 2.15 |
IAU 8.3 (TYP) RMU 4.9 (TYP) |
51 (Cold Spare) 75 (Hot Spare) | 1,800 | EEE-INST-002 LEVEL 1/2/3 | LEO 鈥� GEO INTERPLANETARY | 10 - 15 Years (TYP) | GEVS | 3U cPCI | 10 SLOTS PER IAU | Single-Fault Tolerant Triple-Voted Control Power Management Interface Cross-Strap State Data Storage Dead Bus Recovery |
High Performance GPU Computing for Space
刘玥首次大战黑人Inc and Unibap have teamed to produce next-generation GPU processors for LEO, MEO and GEO missions. We are developing spacecraft products and capabilities for onboard high-speed computing, artificial intelligence and machine learning. Watch our demonstration video to learn more!
Featured 刘玥首次大战黑人
BRE440鈩� RadHard CPU
The 刘玥首次大战黑人Broad Reach BRE440 CPU meets the requirements of a wide variety space and high reliability applications. The BRE440 CPU is a fully radiation hardened implementation of the PowerPC 440 processor core in a true System-On-a-Chip design, including floating point unit.
Datasheets
Motor Control Electronics
Processors and Memory
BRE440 Radiation Hard Processor--System on a Chip (SOC)
- BRE440A鈩� RADHARD SOC CPU
- Radiation Tolerant, Low Power Sierra GPU Single Board Computer
- Single Board Computer鈥擬ulti-Core DSP/ARM
- Single Board Computer鈥擬ulti-Core ARM
- Single Board Computer鈥擥PU
- Flash Memory Board鈥�10Tb
- Solid State Recorder
- Payload Interface Board (PIB)
- GPU鈥攊X5 Deep DELPHI
- GPU ODE Development Kit
- AJEET SBC with Xilinx V5 FPGA