Characteristics:

Propellant components: Hydrogen Peroxide and Kerosene

Thrust (in vacuum): 3,500 N

Exhaust velocity (in vacuum): 3,004 m/s

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Characteristics:

Propellant components: Hydrogen Peroxide and Kerosene

Thrust (in vacuum): 85.5 kN (8.1 tons)

Exhaust velocity (in vacuum): 3,001 m/s

Specific impulse (in vacuum): 306.02 s

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Characteristics:

Propellant components: Hydrogen Peroxide and Kerosene

Thrust per engine:

       70 kN (7 tons) (at sea level)
       79.7 kN (8 tons) (in vacuum)
Exhaust Velocity:

       2,454 m/s (at sea level)

       2,794 m/s (in vacuum)

Specific impulse:

       250.24 s (at sea level)

       284.91 s (in vacuum)

ORBITAL LAUNCH VEHICLE

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