Assuming that the atmosphere has the same density anywhere as at sea level `(rho =1.3 kgm^(-3))` and g to be constant `(g=10 ms^(-2))`. What should be the approximate height of atmosphere ?
`(rho_(0)=1.01xx10^(5)Nm^(-2))`

The density of the atmosphere at sea level is 1.29 kg//m^(3) . Assume that it does not change with altitude, how high should the atmosphere extend?

The density of the atmosphere at sea level is 1.29 kg//m^(3) . Assume that it does not change with altitude, how high should the atmosphere extend?

The density of the atmosphere ats ea level is 1.31kg//m^(3) . Assume that it does not change with altitude . The how high would the atmosphere extend ? (g=10ms^(-2))

The density of the atmosphere at sea level is 1.29kg//m^(3) . Assume that it does not change with altitude . Then how high would the atmosphere extended ? (g=9.8ms^(-2))

Calculate height (Approx) of atmosphere considering density of atmosphere is uniform (rho = 1.3 kg//m^3)

Calculate height (Approx) of atmosphere considering density of atmosphere is uniform (rho = 1.3 kg//m^3)

At sea level, the atmospheric pressure is 1.04 xx 10^5 Pa. Assuming g = 10 "m s"^(-2) and density of air to be uniform and equal to 1.3 "kg m"^(-3) , find the height of the atmosphere.

The density of the atmosphere at sea level is 1.29 kg//m^(3) . Assume that it does not change with altitude. Then how high would the atmosphere extend ? g=9.8 ms^(-2) . Atmospheric pressure =1.013 xx 10^(5) Pa .

The density of the atmosphere at sea level is 1.29 kg//m^(3) . Assume that it does not change with altitude. Then how high would the atmosphere extend ? g=9.8 ms^(-2) . Atmospheric pressure =1.013 xx 10^(5) Pa .

The density of air near the earth's surface is 1.3kg m^-3 and the atmosphere pressure is 1.0xx10^5Nm^-2 . If the atmosphere has uniform density, same as that observed at the surface of the earth , what would be the height of the atmosphere to exert the same pressure .