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gptkbp:instanceOf
|
computer
|
|
gptkbp:dataUsage
|
Magnetic core memory
|
|
gptkbp:designedBy
|
gptkb:MIT_Instrumentation_Laboratory
|
|
gptkbp:developer
|
1966
$150 million
|
|
gptkbp:firstFlight
|
gptkb:Apollo_11
|
|
gptkbp:function
|
navigation
guidance
control
|
|
gptkbp:historicalSignificance
|
First computer used in space missions
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Apollo Guidance Computer
|
|
gptkbp:influenced
|
modern avionics
|
|
gptkbp:influencedBy
|
gptkb:Project_Gemini
|
|
gptkbp:inputOutput
|
Switches
Lights
Displays
Dials and switches
Dials
1.024 Kbps
|
|
gptkbp:language
|
gptkb:AGC_assembly_language
|
|
gptkbp:legacy
|
Paved the way for future space computers
|
|
gptkbp:monitors
|
CRT display
|
|
gptkbp:netIncome
|
RTCC
|
|
gptkbp:notableFeature
|
Real-time computing
Integrated circuits
Low power consumption
Redundancy
High reliability
Fault tolerance
Lightweight construction
User programmability
Modular_design
|
|
gptkbp:operatingHours
|
Executive_and_Luminary
|
|
gptkbp:operationalStatus
|
Spacecraft
|
|
gptkbp:performance
|
1 in 100,000
|
|
gptkbp:powers
|
55 watts
|
|
gptkbp:primaryUser
|
Apollo_Guidance_Computer_User's_Guide
|
|
gptkbp:processor
|
custom integrated circuits
|
|
gptkbp:productionCompany
|
1961
Display and lights
|
|
gptkbp:RAM
|
core rope memory
|
|
gptkbp:reliability
|
High
|
|
gptkbp:succeededBy
|
1 MHz
|
|
gptkbp:successor
|
Space Shuttle Guidance Computer
|
|
gptkbp:teamAchievements
|
gptkb:Margaret_Hamilton
|
|
gptkbp:usedIn
|
gptkb:Saturn_V
gptkb:Apollo_program
Saturn IB
|
|
gptkbp:user_interface
|
AGC_display_and_keyboard
|
|
gptkbp:uses
|
gptkb:Apollo_14
gptkb:Apollo_16
gptkb:Apollo_15
gptkb:Apollo_17
gptkb:Apollo_12
|
|
gptkbp:weight
|
32 kg
|