Gemini Guidance Computer

Gemini Guidance Computer

Gemini Guidance Computer in National Air and Space Museum
Invented by IBM Federal Systems Division
Manufacturer IBM Federal Systems Division
Introduced 1965 (1965)
Discontinued 1966 (1966)
Type Avionics
Guidance Computer
Processor Discrete IC RTL based
Frequency 7.143 kilohertz clock
Memory 39-bit words memory, each composed of three 13-bit syllables, 4096 words of memory, in a ferrite core array.
Ports Modular Display Keyboard (MDK), Modular Display Readout (MDR), Attitude Control and Maneuver Electronics (ACME), Inertial Measurement Unit (IMU), Horizon Sensors, Time Reference System (TRS)[1]
Power consumption 28V DC
Weight 58.98 pounds (26.75 kg)
Dimensions 18.9"(H)×14.5"(W)×12.75"(D)

The Gemini Guidance Computer (sometimes Gemini Spacecraft On-Board Computer (OBC)) was a digital, serial computer designed for Project Gemini, America's second manned space project.[2] The computer, which facilitated the control of mission maneuvers, was designed by the IBM Federal Systems Division.[3]

Functionality

The Gemini Guidance Computer was responsible for the following functions:[3][2]

Specs

References

  1. http://www.ibiblio.org/apollo/Gemini.html#Peripheral_Devices
  2. 1 2 McDonnell Corporation, NASA Project Gemini Familiarization Manual, 1965, vol. 2, pp. 8.7,8.45.
  3. 1 2 8. J. C. Hundley and R. A. Watson, "A Digital Computer in Orbital Flight," TR 63-825-892, IBM Federal Systems Division, Owego, New York, October 1964.
  4. 1 2 "Gemini Spacecraft Computer (OBC): Layout of Memory Words". 2016 [2011]. Archived from the original on 2016-05-28. Retrieved 2016-05-28.
  5. LVDC board reverse engineering project
  6. Computers in Spaceflight: The NASA Experience, chapter one

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