Starship V2

Retired

SpaceX · 2-stage orbital rocket · Part of the Starship family

Total Launches

Success Rate

—

Payload to LEO

100 t

First Flight

2025

Reusable

Yes

Interactive Model

Height121.4 m

Diameter9 m

Wet Mass5,200,000 kg

Payload to GTON/A

Payload to SSON/A

ManufacturerSpaceX

CountryUnited States

Engine usage data lives in the Engine Dashboard.

No launches attributed to this vehicle in the database yet.

Reliability data not available yet.

Specifications

GCAT / Wikipedia · verified quarterly

Launch History

LL2 API · updated every 6h

Engine Data

Manufacturer + Wikidata