DBSE
Hardware/Vehicles/Titan 403B

Titan 403B

Retired

Lockheed Martin · 2-stage orbital rocket · Part of the Titan family

Total Launches
1
Success Rate
100%
Payload to LEO
21.7 t
First Flight
2000
Reusable
No

Specifications

Height54 m
Diameter3.05 m
Wet Mass910,000 kg
Payload to GTON/A
Payload to SSON/A
ManufacturerLockheed Martin
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 IIIEVehicle familyTitan 34DVehicle familyTitan 401B/CentaurVehicle familyLockheed MartinManufacturerUA1207Engine

Data Sources for This Record

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