new design of Saturn 14 rocket with mass 1.79 x106 kg has a propulsion engine that can eject gases at a constant speed of 380.33 m/s (vGas) by burning fuel at a rate of 4.23  x10 5  kg/s (dmdT). In full tank, the rocket can carry a fuel of mass 48.74  x10 6  kg. If this design exceeds the velocity of 11,200 m/s it can successfully escape Earth's gravity. Determine if this is so. Find its maximum velocity (velyZ) in a PhysLab virtual simulation. (Pitch Angle = 0)

A new design of Saturn 14 rocket with mass 1.73 x106 kg has a propulsion engine that can eject gases at a constant speed of 268.8 m/s (vGas) by burning fuel at a rate of 2.77  x10 5  kg/s (dmdT). In full tank, the rocket can carry a fuel of mass 45.04  x10 6  kg. If this design exceeds the velocity of 11,200 m/s it can successfully escape Earth's gravity. Determine if this is so. Find its maximum velocity (velyZ) in a PhysLab virtual simulation. (Pitch Angle = 0)

A new design of Saturn 11 rocket with mass 1.31 x106 kg has a propulsion engine that can eject gases at a constant speed of 339.79 m/s (vGas) by burning fuel at a rate of 3.02  x10 5  kg/s (dmdT). In full tank, the rocket can carry a fuel of mass 44.36  x10 6  kg. If this design exceeds the velocity of 11,200 m/s it can successfully escape Earth's gravity. Determine if this is so. Find its maximum velocity (velyZ) in a PhysLab virtual simulation. (Pitch Angle = 0)

(COLLAB) A new design of Saturn 12 rocket with mass 1.67 x106 kg has a propulsion engine that can eject gases at a constant speed of 387.39 m/s (vGas) by burning fuel at a rate of 3.69 x10 5 kg/s (dmdT). In full tank, the rocket can carry a fuel of mass 46.78 x10 6 kg. If this design exceeds the velocity of 11,200 m/s it can successfully escape Earth's gravity. Determine if this is so. Find its maximum velocity (velyZ) in a PhysLab virtual simulation. (Pitch Angle = 0)