ABOUT

Suborbital launch vehicle derived from Electron for hypersonic flight testing. Deploys payloads up to 700 kg at velocities from 3 to 7.5+ km/s and altitudes above 80 km. 7 launches with 100% mission success.

SPECIFICATIONS 4
Propellant kerosene
Payload Mass 700 kg
Separation Velocity Km S 3-7.5
Separation Altitude 80 km
TAGS