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{{analog computer
 
{{analog computer
 
|title          = PACE 231R
 
|title          = PACE 231R
|image          = EAI PACE 231R (NASA, 1960).jpg
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|image          =  
|caption        = PACE 231R, NASA/Glenn Research Center, 6/6/1960
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|caption        =  
 
|developer      = [[Electronic Associates]]
 
|developer      = [[Electronic Associates]]
 
|manufacturer  = [[Electronic Associates]]
 
|manufacturer  = [[Electronic Associates]]
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[[File:X-15 Simulator.png|thumb|right|200px|X-15 Simulator]]
 
[[File:X-15 Simulator.png|thumb|right|200px|X-15 Simulator]]
 
In 1956, during the development of the North American X-15, no digital computer had the performance capabilities of delivering flight simulation calculations in real time which is why NASA chose the EAI PACE 231R analog computer instead. Three EAI 231R computers, containing 380 operational amplifiers, 101 function generators, 32 servo amplifiers, and 5 electrical multipliers networked together made up the simulator. The simulator covered 0.2 to 7.0 Mach at altitudes from sea level to 1,056,000 feet. It was not, however, capable of providing meaningful landing simulations. <ref name="x-15">{{cite book|last=Jenkins|first=Dennis|middle=R|title=X-15: Extending the Frontiers of Flight|year=2012|publisher=NASA (EBook)|pages=Chapter 6|ryear=2015|rmonth=12|rday=20|url=http://www.nasa.gov/connect/ebooks/aero_x15_detail.html}}</ref>
 
In 1956, during the development of the North American X-15, no digital computer had the performance capabilities of delivering flight simulation calculations in real time which is why NASA chose the EAI PACE 231R analog computer instead. Three EAI 231R computers, containing 380 operational amplifiers, 101 function generators, 32 servo amplifiers, and 5 electrical multipliers networked together made up the simulator. The simulator covered 0.2 to 7.0 Mach at altitudes from sea level to 1,056,000 feet. It was not, however, capable of providing meaningful landing simulations. <ref name="x-15">{{cite book|last=Jenkins|first=Dennis|middle=R|title=X-15: Extending the Frontiers of Flight|year=2012|publisher=NASA (EBook)|pages=Chapter 6|ryear=2015|rmonth=12|rday=20|url=http://www.nasa.gov/connect/ebooks/aero_x15_detail.html}}</ref>
=== HL-10===
 
[[File:HL-10 flight simulator, NASA, 1968.jpg|left|thumb|200px|HL-10 Flight Simulator.]]
 
Flight Research Center's first HL-10 simulations was done with the PACE 231R. As they described "The real capability of the analog computer was its ability to integrate differential equations. Because the equations of motion for the lifting bodies were differential equations-as are all equations of motion for aerospace vehicles-the simulation engineers mechanized them on available analog computers."<ref name="nasa1">{{apa web|last=Reed|first=Dale|middle=R.|month=August|year=1997|title=BACK TO THE DRAWING BOARD|web title =SP-4220 Wingless Flight: The Lifting Body Story|rmonth=12|rday=22|ryear=2015|url=http://history.nasa.gov/SP-4220/ch6.htm}}</ref>
 
{{clear}}
 
 
===Langley Research Center / Project Mercury===
 
===Langley Research Center / Project Mercury===
 
In June 1960 EAI won a $1.51M contract to supply NASA's Langley Research Center with five fully expended PACE 231R systems. Those systems were used for various aspects of the Mercury project, including space station rendezvous. It was also used for  the simulation of missile launches and satellites.<ref name="b1" />
 
In June 1960 EAI won a $1.51M contract to supply NASA's Langley Research Center with five fully expended PACE 231R systems. Those systems were used for various aspects of the Mercury project, including space station rendezvous. It was also used for  the simulation of missile launches and satellites.<ref name="b1" />
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== References==
 
== References==
 
{{reflist}}
 
{{reflist}}
 
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