thrust

Mass: 2000 kg: Vel = 0 km/s: acc = 0.00 m/s^2


 Display Data

time,mass,v,a

Rocket mass = 1200 kg

Fuel mass = 800 kg

Burn Rate = 20 kg/s

Vexh= 1470 m/s
Rocket equation delta v:

Vel: 0.751 km/s
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