Single Board Computer (SBC) Family
Cobham Semiconductor Solutions introduces our off-the-shelf Single Board Computer family.
With our Electronic Manufacturing Service (EMS) experience on the LEAP and various flight board builds, Cobham can serve your needs with an off-the-shelf Single Board Computer (SBC) option specifically designed for Command and Control Applications.
Our first is a GEN 6 LEON 3FT - a flight ready TRL-8 SBC for LEO, GEO and Planetary Missions.
- Flexible Architecture
- Enabled for use of LEON 3FTs Microprocessors - UT699, UT699E, UT700
- Up to 95 Dhrystone MIPS performance with 132MHz System Clock
- 64MB of SRAM Memory
- 4 of Cobham 160Mb SRAMs
- 32MB of NV Memory
- 5 of Cobhams 64Mb MRAMs
- Two cPCI bus I/F connectors (Hypertronics)
- Two SpW connectors and front panel test connector
- IPC-6012 Class 3A compliance
- Analyses completed as of 4-2015
- MTBR Rel Analysis
- Component Radiation
- FMEA on all components and failure modes
- Signal Integrity
- Timing analysis
- TRL-8 board qualification completed
The GEN 6 SBC is available now for your missions!
For questions, please call 800-645-8862.
Available Single Board Computer Products
|Single board Computer (SBC) Products|
|Memory Access (MHz)/
|DS4350272-x00||UT699E||33||33||33 / 0 W-S||44.2||33||3.0||5.1|
|DS4350272-x01||UT699E||66||66||66 / 3 W-S||70.4||132||3.5||6.6|
|DS4350272-x02||UT700||33||33||33 / 0 W-S||44.2||33||3.0||5.1|
|DS4350272-x03||UT700||66||66||66 / 3 W-S||70.4||132||3.5||6.6|
|DS4350272-x04||UT700||132||66||66 / 3 W-S||94.9||132||4.2||7.3|
|DS4350272-x05||UT699||49.5||49.5||49.5 / 3 W-S||50.9||99||5.5||8.5|
|Conditions: cPCI active/Memory Access [Typ = no Access | Max = 50%|
All other IP Functions Disabled via Clock gating register.
|GEN VI Single Board Computer EM, FM Designations|
Several models of the GEN VI SBCs can be manufactured based on usage purpose, delivery schedule, mass, and cost.
The following types of assemblies are identified:
a) Flight Modules (FM): Designated by a -3xx in the part number, the FMs are used in spacecraft final production. These units meet full specifications.
b) Engineering Model (EM): Designated by a -1xx in the part number, the EMs are flight-like units used in the flight design checkout, software development and qualification, upper assembly unit checkout and initial flight unit integration (pre-environmental). EMs meet full design specifications less the Flight Parts and board level environmental tests/screening.