The integrated electronic products cover with single machine functions, such as data management, attitude and orbit control computer, telecontrol, telemetry terminal, power supply, propulsion and thermal control lower computer. It is possible to quickly and agilely compose a integrated aerospace electronic subsystem through modularization and generalization and mutually connected by standard bus and hardware .

Chinese 1750 series of data-management/ housekeeping/control/ center computer

l CPU: SM1750  (made in China)

l  Main frequency: 10～20MHz

l  processing capability: 3～5MIPS

l  Storage capability  

             PROM: 128kB

             SRAM: 1MB (EDAC)

             EEPROM: 768kB (EDAC)

l  Inner bus  protocol: ISA protocol

l  Outer bus:  1553B bus, SpaceWire bus

l  interface:   RS422, LVDS, AD/DA, OC gate output

l  Solid-state storage capability: 64Gbits~128Gbits (Flash)

l  Data transmission mode: RS code, according with CCSDS standard

l  Power consumption: <28W

l  Weight: ≤9.5kg

l  Size: 256mm×324mm×197mm

l  Development period:  T0+8 months