Payload LEO
1,000 kg
Payload SSO
700 kg
Assessment
Two-stage launch vehicle (LOX/propane, 9 first-stage engines, 1 Aquila upper-stage engine) for small and medium satellites; maiden flight in March 2025, still in the test-flight/development phase.
Technical data
Height28 m
Diameter2 m
Liftoff thrust675 kN
Stages2
PropellantLOX/propane
ReusabilityExpendable
First flight2025
Lead time–
Provider launch sites
Andøya SpaceportGuiana Space Centre – Diamant (Kourou)Spaceport Nova Scotia
Price
Price on requestPrices shown are the providers' official figures and are always non-binding – only the individual quote is binding.