Voyager 1 electrical power subsystem

E870144

The Voyager 1 electrical power subsystem is the spacecraft’s radioisotope thermoelectric generator–based system that supplies and manages electrical power for all onboard instruments and systems throughout its deep-space mission.

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Statements (50)

Predicate Object
instanceOf spacecraft electrical power subsystem
spacecraft subsystem
cannotUse solar arrays
designedFor autonomous operation
deep-space mission
high reliability
long-duration operation
redundancy
developedBy Jet Propulsion Laboratory NERFINISHED
NASA NERFINISHED
environment deep space
interstellar space
exceededDesignLifetime true
hasComponent RTG power conversion units
battery (for transient loads only)
cabling and harnesses
fuses and circuit protection devices
load switching circuitry
power control electronics
power distribution unit
voltage regulation circuitry
initialElectricalPowerOutput approximately 470 watts at launch
initialNumberOfRTGs 3
launchDate 1977-09-05
lifetimeDesignGoal at least 5 years
managesPowerFor Voyager 1 attitude control system NERFINISHED
Voyager 1 communication system
Voyager 1 data handling system
Voyager 1 science instruments NERFINISHED
Voyager 1 thermal control system
mission Voyager 1 interstellar mission NERFINISHED
Voyager program NERFINISHED
mustOperateAt large heliocentric distances
partOf Voyager 1 NERFINISHED
poweredBy Pu-238 radioisotope fuel
plutonium-238
powerOutputDecreasesDueTo radioactive decay of Pu-238
thermocouple degradation
providesPowerTo attitude thruster valves
heaters for thermal control
onboard computers
radio receivers
radio transmitters
reasonForRTGUse insufficient solar flux at outer planets and beyond
stillOperationalAsOf 2024
supports load shedding strategies
power margin management
selective instrument shutdown to conserve power
uses RTG NERFINISHED
radioisotope thermoelectric generators

Referenced by (1)

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Voyager 1 flight data system powerSource Voyager 1 electrical power subsystem