(COLLAB) A new design of Satum 14 rocket with mass 1.84 x106 kg has a propulsion engine that can eject gases at a constant speed of 248.98 m/s (vGas) by burning fuel at a rate of 3.22 x10 5 kg/s (dmdT). In full tank, the rocket can carry a fuel of mass 45.32 x10 b 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 Satum 14 rocket with mass 1.84 x106 kg has a propulsion engine that can eject gases at a constant speed of 248.98 m/s (vGas) by burning fuel at a rate of 3.22 x10 5 kg/s (dmdT). In full tank, the rocket can carry a fuel of mass 45.32 x10 b 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)
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A new design of Saturn 14 rocket with mass 1.84 × 10^6 kg has a propulsion engine that can eject gases at a constant speed of 248.98 m/s (vGas) by burning fuel at a rate of 3.22 × 10^5 kg/s (dmdT). In full tank, the rocket can carry a fuel of mass 45.32 × 10^6 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)
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