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Hardware/Vehicles/Titan IIIE

Titan IIIE

Retired

Martin Marietta · 3-stage orbital rocket · Part of the Titan family

Total Launches
7
Success Rate
85.7%
Payload to LEO
14 t
First Flight
1974
Reusable
No

Interactive Model

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Specifications

Height48.8 m
Diameter3.05 m
Wet Mass633,000 kg
Payload to GTON/A
Payload to SSON/A
ManufacturerMartin Marietta
CountryUnited States

Engines Used

Engine usage data lives in the Engine Dashboard.

Launch History

Reliability by Year

Related Entities

Titan II GLVVehicle familyTitan IIICVehicle familyTitan 34DVehicle familyTitan 403BVehicle familyTitan 401B/CentaurVehicle familyMartin MariettaManufacturerUA1207Engine

Data Sources for This Record

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