how high would the atmosphere extend if it were of uniform density throughout, equal to half the present density at sea level?

Let H be that height.

Solve this equation for h

Po = (1/2)(rho0) g H

Po = 1.01*10^5 N/m^2
(rho0) = sea level average density of air = (approx) 1.2*10^3 kg/m^3
g = 9.8 m/s^2

http://en.wikipedia.org/wiki/Atmospheric_pressure

Well, if the atmosphere were of uniform density throughout and equal to half the present density at sea level, it would extend all the way into outer space, giving you a whole new meaning to the term "sky's the limit"! But hey, think of the view you'd have from up there. Just make sure to pack a good pair of binoculars and a spacesuit with a sense of humor.

To determine how high the atmosphere would extend if it were of uniform density throughout, equal to half the present density at sea level, we can use the concept of atmospheric pressure and the barometric formula.

The barometric formula relates the pressure at a given altitude to the density of air and the acceleration due to gravity. It is expressed as:

P = P₀ * exp(-M * g * h / (R * T))

Where:
P is the pressure at altitude h
P₀ is the pressure at sea level
M is the molar mass of Earth's air (approximately 0.029 kg/mol)
g is the acceleration due to gravity (approximately 9.8 m/s²)
h is the altitude
R is the ideal gas constant (approximately 8.314 J/(mol·K))
T is the absolute temperature in Kelvin

Assuming the present density at sea level is ρ₀, and the uniform density throughout the atmosphere is ρ = ρ₀ / 2, we can rewrite the barometric formula as:

P = P₀ * exp(-ρ * g * h / (2 * R * T))

We want to find the altitude at which the pressure drops to zero. Therefore, we can set P = 0 and solve for h:

0 = P₀ * exp(-ρ * g * h / (2 * R * T))

Dividing both sides of the equation by P₀ and taking the logarithm of both sides, we have:

0 = -ρ * g * h / (2 * R * T)

Re-arranging the terms, we get:

h = - (2 * R * T) / (ρ * g)

Substituting ρ = ρ₀ / 2, we have:

h = - (4 * R * T) / (ρ₀ * g)

The value of T and g can be approximated as constant, so we can simplify the equation as:

h = constant / ρ₀

Therefore, the height at which the atmosphere would extend if it were of uniform density throughout, equal to half the present density at sea level, is inversely proportional to the present density at sea level. As the density decreases, the height would increase.

To determine how high the atmosphere would extend if it were of uniform density throughout, equal to half the present density at sea level, you need to consider the concept of atmospheric pressure.

The height to which the atmosphere extends is determined by the balance between gravity and atmospheric pressure. At sea level, the density of the atmosphere decreases as you go higher. If the atmosphere were to have a uniform density, it would mean that the pressure would also decrease uniformly with height.

We can use the hydrostatic equilibrium equation, which relates pressure, density, and height, to find the answer. The equation is:

P = ρ * g * h

Where:
P is the pressure at a given height,
ρ is the density of the air,
g is the acceleration due to gravity, and
h is the height.

The given condition states that the density is half the present density at sea level. Let's define the present density at sea level as ρ_0. So, the density in this scenario would be ρ = 0.5 * ρ_0.

Now, let's assume that the height to which the atmosphere extends is h. We can express the pressure at sea level (P_0) and at the top of the atmosphere (P_top) using the equation:

P_0 = ρ_0 * g * 0 (since height at sea level is 0)
P_top = ρ * g * h

Since the density is half at each point, we can write:

P_0 = (0.5 * ρ_0) * g * 0 = 0
P_top = (0.5 * ρ_0) * g * h

From this, we can conclude that P_top = 2 * P_0.

However, we know that the pressure at the top of the atmosphere is effectively 0 (outer space). Therefore, we equate P_top = 0 and solve for h:

0.5 * ρ_0 * g * h = 0
h = 0

This means that in the given scenario where the atmosphere is of uniform density equal to half the present density at sea level, the atmosphere would extend to a height of 0 meters (or effectively no height).