Standardized modular instrumentation system for space scientific instruments

Details Standardized modular instrumentation system for space scientific instruments Standardized modular instrumentation system for space scientific instruments

Feb 1977

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1977itns...24..823c&link_type=abstract

(IEEE, ERDA, NASA, and NBS, Nuclear Science Symposium, 23rd, Scintillation and Semiconductor Counter Symposium, 15th, and Nuclea

Computer Science

Airborne/Spaceborne Computers, Electronic Modules, Microprocessors, Signal Processing, Spacecraft Instruments, Systems Engineering, Architecture (Computers), Command And Control, Computer Systems Design, Data Links, Hybrid Computers

Scientific paper

A standardized instrument modular system, similar in concept to NIM/CAMAC, is described. Programmable analog and digital functional blocks are contained within hybrid 'nodes'. Up to twelve of these nodes of any desired mix are mounted on standard modules which, in turn, are housed in a modified CAMAC crate. A station control on each module allows access of CAMAC control functions and/or data transfers from the dataway into each node. CAMAC protocol is used in the crate controller and branch driver. A micro-computer controls data handling and spacecraft command and telemetry interfaces.

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