Titan 401B/Centaur
RetiredLockheed Martin · 3-stage orbital rocket · Part of the Titan family
Total Launches
0
Success Rate
—
Payload to LEO
—
First Flight
—
Reusable
No
Specifications
Height62.2 m
Diameter3.05 m
Wet Mass939,000 kg
Payload to GTO9 t
Payload to SSON/A
ManufacturerLockheed Martin
CountryUnited States
Engines Used
Engine usage data lives in the Engine Dashboard.
Launch History
No launches attributed to this vehicle in the database yet.
Reliability by Year
Reliability data not available yet.
Related Entities
Data Sources for This Record
Specifications
GCAT / Wikipedia · verified quarterly
Launch History
LL2 API · updated every 6h
Engine Data
Manufacturer + Wikidata