Saturn V instrument unit

E551351

The Saturn V instrument unit was the ring-shaped electronic control and guidance section that housed the rocket’s navigation, telemetry, and flight control systems.

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Observed surface forms (1)

Surface form Occurrences
Saturn V Instrument Unit 0

Statements (53)

Predicate Object
instanceOf avionics ring
rocket guidance system
space launch vehicle component
contains environmental control equipment
guidance computer
inertial measurement unit
power distribution systems
radio communication equipment
sequencer electronics
stabilization and control system electronics
telemetry systems
tracking and data systems interfaces
developedBy Marshall Space Flight Center NERFINISHED
NASA NERFINISHED
diameter approximately 6.6 meters
firstFlight Apollo 4 NERFINISHED
firstFlightDate 1967-11-09
guidanceComputer IBM Launch Vehicle Digital Computer NERFINISHED
height approximately 0.9 meters
inertialPlatform ST-124-M3 inertial measurement unit
locatedAt top of Saturn V S-IVB stage
mass approximately 2,000 kilograms
partOf Saturn V NERFINISHED
primaryContractor IBM NERFINISHED
program Apollo program NERFINISHED
Skylab program NERFINISHED
shape ring-shaped
usedFor attitude control
engine cutoff control
engine ignition control
flight control
guidance
navigation
pitch control
roll control
sequencing of Saturn V events
staging control
telemetry
yaw control
usedOn Apollo 10 NERFINISHED
Apollo 11 NERFINISHED
Apollo 12 NERFINISHED
Apollo 13 NERFINISHED
Apollo 14 NERFINISHED
Apollo 15 NERFINISHED
Apollo 16 NERFINISHED
Apollo 17 NERFINISHED
Apollo 4 NERFINISHED
Apollo 6 NERFINISHED
Apollo 8 NERFINISHED
Apollo 9 NERFINISHED
Apollo–Soyuz Test Project Saturn IB (variant design)
Skylab 1 launch NERFINISHED

Referenced by (1)

Full triples — surface form annotated when it differs from this entity's canonical label.

S-IC guidanceSystemLocation Saturn V instrument unit