DBSE
Hardware/Vehicles/Antares 230

Antares 230

Retired

Northrop Grumman · 2-stage orbital rocket · Part of the Zenit family

Total Launches
0
Success Rate
—
Payload to LEO
6.3 t
First Flight
2016
Reusable
No

Interactive Model

Open full size →

Specifications

Height42.5 m
Diameter3.9 m
Wet Mass290,000 kg
Payload to GTO1.8 t
Payload to SSON/A
ManufacturerNorthrop Grumman
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

Zenit-2Vehicle familyZenit-3SLVehicle familyZenit-3SLBVehicle familyAntares 110Vehicle familyAntares 120Vehicle familyAntares 130Vehicle familyAntares 230+Vehicle familyRD-181Engine

Data Sources for This Record

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