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Spacecraft Computer Development Prototype

RH32  Spacecraft Computer Prototype Development Unit

 

 

Features

Applications

· H32 RISC CPU with variable clock

· 4Mbyte local SRAM, 512 Kbyte EEPROM, 96 Kbytes trace/fault log NVRAM, 12 Mbyte dual ported global SRAM

· Backplane can be configured as RH32 Bus, Module Bus or VME Bus

·RS-232, IEEE-488, IEEE 1149.1 Mil-STD 1553B and Ethernet interfaces

· Bus history recorder, hardware trap, and fault log capability

· Real-time debug control

· Single or Multiple processor architecture

· Fully supported by major software toolset vendors

· Low cost concept evaluation, architecture studies and system validation

·Software development and debug before and after flight hardware availability

· Configurable as functional equivalent unit for RH32 flight systems

· Flight computer test station

· Single or multiple processor architecture

· Fully supported by major software toolset vendors

 

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