Voyager 2 telecommunications subsystem

E850197

The Voyager 2 telecommunications subsystem is the spacecraft’s radio and antenna system that sends scientific data and status information across interplanetary distances back to Earth and receives commands from mission control.

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Statements (49)

Predicate Object
instanceOf deep-space communications system
spacecraft telecommunications subsystem
communicatesOver interplanetary distances
interstellar distances
communicatesWith Earth-based ground stations
designedFor deep-space communication
interplanetary communication
designedIn 1970s
developedBy Jet Propulsion Laboratory NERFINISHED
enables data return from Jupiter flyby
data return from Neptune flyby
data return from Saturn flyby
data return from Uranus flyby
function receive commands from Earth
send engineering and status data to Earth
send scientific data to Earth
includes command subsystem interface
demodulator
high-gain antenna
low-gain antenna
medium-gain antenna
modulator
radio frequency subsystem
receiver
telemetry subsystem interface
transmitter
launchDate 1977-08-20
launchVehicle Titan IIIE-Centaur NERFINISHED
location Voyager 2 spacecraft body NERFINISHED
mission Voyager program NERFINISHED
missionPhase interstellar mission phase
planetary flyby phase
operatedBy NASA
orientation fixed to high-gain antenna structure
partOf Voyager 2 NERFINISHED
poweredBy Voyager 2 power subsystem
receivesFrom Deep Space Network NERFINISHED
spacecraftBus Voyager bus
status operational (as of 2024)
supports command uplink
radio science experiments
ranging
telemetry downlink
transmitsTo Deep Space Network NERFINISHED
uses S-band NERFINISHED
X-band
coherent transponding
phase-coherent two-way communication
radio frequency communication

Referenced by (1)

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Voyager 2 attitude control system coordinatesWith Voyager 2 telecommunications subsystem