THE ROCKET FUELER
Thrust
0 kN
Velocity
0 m/s
ABORT
Propellant Mix
Mix Ratio (Oxidizer / Fuel)
50% Ox / 50% Fuel
Combustion Fact

Stoichiometric ratio ensures complete combustion for maximum efficiency.

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Telemetry
Altitude
0 km
Status
Grounded
System initialized...
Awaiting ignition sequence...
Adjust mixture and ignite...