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Hardware/Vehicles/Antares 230+

Antares 230+

On Hold

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

Total Launches
13
Success Rate
100%
Payload to LEO
6.3 t
First Flight
2016
Reusable
No

Interactive Model

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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

Reliability by Year

Related Entities

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

Data Sources for This Record

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