A new design of Saturn 12 rocket with mass 1.2 x106 kg has a propulsion engine that can eject gases at a constant speed of 363.9 m/s (vGas) by burning fuel at a rate of 2.01  x10 5  kg/s (dmdT). In full tank, the rocket can carry a fuel of mass 45.96  x10 6  kg. If this design exceeds the velocity of 11,200 m/s it can can successfully escape Earth's gravity. Determine if this is so. Find its maximum velocity (velyZ). (Pitch Angle = 0)

A new design of Saturn 17 rocket with mass 1.82 x106 kg has a propulsion engine that can eject gases at a constant speed of 335.12 m/s (vGas) by burning fuel at a rate of 4.14  x10 5  kg/s (dmdT). In full tank, the rocket can carry a fuel of mass 47.09  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 1.61 x106 kg has a propulsion engine that can eject gases at a constant speed of 365.82 m/s (vGas) by burning fuel at a rate of 4.68  x10 5  kg/s (dmdT). In full tank, the rocket can carry a fuel of mass 47.95  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 11 rocket with mass 1.62 x106 kg has a propulsion engine that can eject gases at a constant speed of 379.94 m/s (vGas) by burning fuel at a rate of 2.85  x10 5  kg/s (dmdT). In full tank, the rocket can carry a fuel of mass 44.39  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) (Please express the final answer without rounding off and without scientific notation)