When the gravitational and drag forces on the object are equal, there is no net force acting on the object. This means that the body will not accelerate; it will not change it's velocity.
In order for the body to slow down to "floating speed", the drag force would have to be greater than the gravitational force. Drag force is dependent on velocity though, so the greater the velocity the greater the drag. Since the body is not accelerating at terminal velocity, it won't increase it's velocity, and therefore the drag force on it will not increase.
(This is all assuming that is a rigid body in an atmosphere with a more or less uniform density, such as a block falling from an airplane.)
4h
Zero
A rocket that doesn't reach "escape velocity" will be overcome by gravity and will be pulled back down to Earth. Also, rockets which go into orbit have not reached escape velocity. Escape velocity is what is needed to completely leave earth's gravity well.
There is not enough information to answer the question. The initial velocity of the car is not given. Also, the "it finally" at the end of the question does not make sense.
The average acceleration is given by the expression a ∆v/∆t (15 m/s)/5s 3m/s2 where a is acceleration, v is velocity, and t is time. ∆ (final-initial) value.
Fluorine attains the electron configuration of neon (the nearest noble gas).
No the theory of relativity clearly states that it is impossible for any body with mass to attain light velocity m = m0/(1 - v/c)1/2 from this it is clear that if a body attains light velocity its mass will be infinity which is impossible.
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"Escape velocity" is a myth, a poorly understood fiction. "Escape velocity" is the initial velocity needed for a projectile WHEN FIRED if you want the projectile to leave the Earth entirely. Rockets, which can accelerate for a long period, never need to come anywhere close to the Earth's escape velocity of 7 miles per second in order to leave the Earth behind. However, in order to attain a stable orbit, satellites do need to accelerate to fairly high velocities; about 18,000 miles per hour in low orbit, somewhat more slowly in higher orbits.
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From that information we could determine its kinetic energy from the formula K.E. = ½mv² ½ x 0.14 kg x (18 m/s)² = 22.687 kg·m²/s² = 22.687 Joules
The average acceleration can be calculated using the equation of motion: average acceleration = (final velocity - initial velocity) / time. Plugging in the values, we get: average acceleration = (26.3 m/s - 0 m/s) / 0.59 s ≈ 44.6 m/s^2.