DBSE
Hardware/Vehicles/Antares 120

Antares 120

Retired

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

Total Launches
2
Success Rate
100%
Payload to LEO
4.6 t
First Flight
2014
Reusable
No

Specifications

Height40.5 m
Diameter3.9 m
Wet Mass282,000 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

Reliability by Year

Related Entities

Zenit-2Vehicle familyZenit-3SLVehicle familyZenit-3SLBVehicle familyAntares 110Vehicle familyAntares 130Vehicle familyAntares 230+Vehicle familyAntares 230Vehicle familyNK-33A (AJ26-62)Engine

Data Sources for This Record

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