Mission Control Center

Design, simulate, and optimize your rocket engine configurations

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Mission Name

Engine Type

Thrust Level (kN)

50 kN

Fuel Mass (kg)

Chamber Pressure (MPa)

Speed0.00 m/s

Distance0.00 km

Altitude0.00 km

Engine Type

Propellant Type

Environment

Propellant Mass (kg)

Nozzle Expansion Ratio

Simulation Duration (s)

Thrust

0.00 kN

Specific Impulse

0 s

Propellant Mass

0 kg

Burn Time

0.0 s

Chamber Temp

0 K

Chamber Pressure

0.00 MPa

Exhaust Velocity

0.0 km/s

Thrust-to-Weight

0.0

Engine Off

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