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Fault-tolerant computing system " PHOENIX"
To solve the problem of creating equipment for a new generation of aerospace systems, a distinctive feature of which is a long period of active existence (15-17 years) and the installation of equipment outside the sealed compartments of the SPACECRAFT, the research Institute "ARGON" has created a technology for the development and manufacture of durable, fault-tolerant and radiation-resistant equipment for special applications. When it was created, the 45-year experience of the research Institute "ARGON" was used to develop on-Board computing facilities for aerospace purposes, advanced technologies and design tools for modern electronic AND radio-electronic devices. The basis of the "DORA" technology is a reliability-oriented design using a unified basic load-bearing structure, certified highly reliable element base, unified circuit and system solutions, a system of defect-free design and testing, proven methods and means of quality control.
Part number:
Description
To solve the problem of creating equipment for a new generation of aerospace systems, a distinctive feature of which is a long period of active existence (15-17 years) and the installation of equipment outside the sealed compartments of the SPACECRAFT, the research Institute "ARGON" has created a technology for the development and manufacture of durable, fault-tolerant and radiation-resistant equipment for special applications. When it was created, the 45-year experience of the research Institute "ARGON" was used to develop on-Board computing facilities for aerospace purposes, advanced technologies and design tools for modern electronic AND radio-electronic devices. The basis of the "DORA" technology is a reliability-oriented design using a unified basic load-bearing structure, certified highly reliable element base, unified circuit and system solutions, a system of defect-free design and testing, proven methods and means of quality control.
Supplier:
JSC "CONCERN OF RADIO ENGINEERING" VEGA"
About the product
DESCRIPTION
The effectiveness of this technology is confirmed by the successful use of more than 150 devices created using this technology in the ISS "ALPHA" and communication satellites "YAMAL-100", "YAMAL-200 ""YAMAL-300K" in 1997-2012.
Currently, the research Institute "ARGON" has started production of the next generation of means of integration of onboard SPACECRAFT devices based on the basic load-bearing structure of BNK-2010. Of interconnecting means on-Board SPACECRAFT equipment is intended for integration of avionics-based network architecture implements the principles of digital platforms and include computing resources, control of power systems, telecommunications and communication adapters with devices SOUD, et al.
The Phoenix fault-tolerant computer system is intended as an integrated computing resource of the onboard SPACECRAFT control system.
To ensure the acceptable recovery time IN the Phoenix OVC, both the spatial and temporal redundancy of the Quad-core structure formed by two two-channel CMOS and interprocessor exchange channels is used
Supplier:
JSC "CONCERN OF RADIO ENGINEERING" VEGA"
About the product
DESCRIPTION
The effectiveness of this technology is confirmed by the successful use of more than 150 devices created using this technology in the ISS "ALPHA" and communication satellites "YAMAL-100", "YAMAL-200 ""YAMAL-300K" in 1997-2012.
Currently, the research Institute "ARGON" has started production of the next generation of means of integration of onboard SPACECRAFT devices based on the basic load-bearing structure of BNK-2010. Of interconnecting means on-Board SPACECRAFT equipment is intended for integration of avionics-based network architecture implements the principles of digital platforms and include computing resources, control of power systems, telecommunications and communication adapters with devices SOUD, et al.
The Phoenix fault-tolerant computer system is intended as an integrated computing resource of the onboard SPACECRAFT control system.
To ensure the acceptable recovery time IN the Phoenix OVC, both the spatial and temporal redundancy of the Quad-core structure formed by two two-channel CMOS and interprocessor exchange channels is used