Payload LEO
16,300 kg
Payload GTO
3,200 kg
Payload Mond
2,300 kg
Assessment
Medium-lift launch vehicle developed jointly with Northrop Grumman (formerly designated MLV); partially reusable first stage. First flight no earlier than 2027 from Wallops Island / MARS, Virginia. Cargo only.
Technical data
Height59 m
Diameter4.3 m
Liftoff thrust7,161 kN
Stages2
PropellantLOX/RP-1
ReusabilityPartially reusable
Lead time–
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