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Hardware/Vehicles/Saturn V

Saturn V

Retired

NASA / MSFC · 4-stage orbital rocket

Total Launches
13
Success Rate
92.3%
Payload to LEO
118 t
First Flight
1967
Reusable
No

Interactive Model

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Specifications

Height110.6 m
Diameter10.06 m
Wet Mass2,913,000 kg
Payload to GTON/A
Payload to SSON/A
ManufacturerNASA / MSFC
CountryUnited States

Engines Used

Engine usage data lives in the Engine Dashboard.

Launch History

Reliability by Year

Related Entities

NASA / MSFCManufacturerF-1Engine

Data Sources for This Record

Specifications
GCAT / Wikipedia · verified quarterly
Launch History
LL2 API · updated every 6h
Engine Data
Manufacturer + Wikidata