DBSE
Hardware/Vehicles/Atlas 3A

Atlas 3A

Retired

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

Total Launches
0
Success Rate
—
Payload to LEO
8.6 t
First Flight
—
Reusable
No

Specifications

Height52.8 m
Diameter3.05 m
Wet Mass225,000 kg
Payload to GTO4.1 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

Atlas CentaurVehicle familyAtlas IVehicle familyAtlas IIVehicle familyAtlas IIAVehicle familyAtlas IIASVehicle familyAtlas 3BVehicle familyLockheed MartinManufacturerRD-180Engine

Data Sources for This Record

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