From WikiChip
Difference between revisions of "dynex/mas31750"

(Created page with "{{Microprocessor |name = Dynex MAS31750 |developer = Dynex |intro_date = 1989 |model = MAS31750 |transistors = |clock =...")
 
m
 
(5 intermediate revisions by 2 users not shown)
Line 1: Line 1:
{{Microprocessor
+
{{dynex title|MAS31750}}{{Microprocessor
 
|name            = Dynex MAS31750
 
|name            = Dynex MAS31750
 
|developer        = [[Dynex]]
 
|developer        = [[Dynex]]
Line 10: Line 10:
 
|gpr              = 16
 
|gpr              = 16
 
|mem_max          = ?
 
|mem_max          = ?
|package          = 64-pin [[BeO]]
+
|package          = 84-pin [[Quad Flat Package|QFP]]<br />84-pin [[Pin grid array|PGA]]
 
}}
 
}}
 
The '''Dynex MAS31750''' is a high-performance, radiation-hardened, 16-bit [[microprocessor]] developed by [[Dynex Semiconductor]]. The chip, which implements the [[MIL-STD-1750A]] standard, has been used in multiple spacecraft missions.
 
The '''Dynex MAS31750''' is a high-performance, radiation-hardened, 16-bit [[microprocessor]] developed by [[Dynex Semiconductor]]. The chip, which implements the [[MIL-STD-1750A]] standard, has been used in multiple spacecraft missions.
Line 17: Line 17:
 
The MAS31750 has been used in multiple spacecrafts missions, including:
 
The MAS31750 has been used in multiple spacecrafts missions, including:
 
* [[Wikipedia:Rosetta (spacecraft)|Rosetta spacecraft]], a robotic spacecraft designed to perform a detailed study of comet [[Wikipedia:67P/Churyumov–Gerasimenko|67P/Churyumov–Gerasimenko]]<ref>[http://www3.imperial.ac.uk/spat/research/areas/space_magnetometer_laboratory/spaceinstrumentationresearch/spaceinstrumentdesign/instrumentcontrolunits Instrument Control Units]; Imperial College London, South Kensington Campus</ref>
 
* [[Wikipedia:Rosetta (spacecraft)|Rosetta spacecraft]], a robotic spacecraft designed to perform a detailed study of comet [[Wikipedia:67P/Churyumov–Gerasimenko|67P/Churyumov–Gerasimenko]]<ref>[http://www3.imperial.ac.uk/spat/research/areas/space_magnetometer_laboratory/spaceinstrumentationresearch/spaceinstrumentdesign/instrumentcontrolunits Instrument Control Units]; Imperial College London, South Kensington Campus</ref>
* [[Wikipedia:Double Star (satellite)|Double Star satellite]], a joined satellite missions by the [[Wikipedia:China National Space Administration|CNSA]] and the [[Wikipedia:European Space Agency|ESA]] to investigate Earth's magnetosphere.
+
* [[Wikipedia:Double Star (satellite)|Double Star satellite]], a joined satellite missions by the [[Wikipedia:China National Space Administration|CNSA]] and the [[Wikipedia:European Space Agency|ESA]] to investigate Earth's magnetosphere.<ref>[http://www.ann-geophys.net/23/2713/2005/angeo-23-2713-2005.pdf The Double Star magnetic field investigation: instrument design, performance and highlights of the first year’s observations]</ref>
 
* [[Wikipedia:Cluster (spacecraft)|Cluster spacecraft]], an [[Wikipedia:European Space Agency|European Space Agency]] spacecraft
 
* [[Wikipedia:Cluster (spacecraft)|Cluster spacecraft]], an [[Wikipedia:European Space Agency|European Space Agency]] spacecraft
 
* [[Wikipedia:Global Ozone Monitoring by Occultation of Stars|GOMOS]], an instrument on board the [[Wikipedia:Envisat|Envisat]] satellite.<ref>Holsti, N. & Pastila, T.; [http://adsabs.harvard.edu/full/1997ESASP.409..323H GOMOS Instrument Pointing Control Software]; Data Systems in Aerospace</ref>
 
* [[Wikipedia:Global Ozone Monitoring by Occultation of Stars|GOMOS]], an instrument on board the [[Wikipedia:Envisat|Envisat]] satellite.<ref>Holsti, N. & Pastila, T.; [http://adsabs.harvard.edu/full/1997ESASP.409..323H GOMOS Instrument Pointing Control Software]; Data Systems in Aerospace</ref>
Line 32: Line 32:
 
[[Category:Dynex Semiconductor microprocessors]]
 
[[Category:Dynex Semiconductor microprocessors]]
 
[[Category:Microprocessor stubs]]
 
[[Category:Microprocessor stubs]]
 +
[[Category:MIL-STD-1750A microprocessors]]

Latest revision as of 16:29, 20 December 2015

Dynex MAS31750
no photo (ic).svg

Developer Dynex

Introduction date 1989

Model MAS31750

Clock 25MHz

Bus Width 16-bit

GPRs 16
Memory Specs
Max Memory  ?

Packaging
Package 84-pin QFP
84-pin PGA

The Dynex MAS31750 is a high-performance, radiation-hardened, 16-bit microprocessor developed by Dynex Semiconductor. The chip, which implements the MIL-STD-1750A standard, has been used in multiple spacecraft missions.

Spacecrafts[edit]

The MAS31750 has been used in multiple spacecrafts missions, including:

References[edit]

External links[edit]