The atmospheric pressure is
and altitude is
.
The rate of change of
with respect to
is proportional to
.

Hence
, where
is a constant.
At the sea level, the pressure is
kpa.
Pressure at an altitude of
is
kpa.
The general equation is
.
Substitute
and
in the above equation.

Substitute
in the
.
Pressure at an altitude
is
.
(a).
\Find the pressure at a altitude of
.
Substitute
in the pressure function
.

The pressure is
kpa at an altitude of
.
(b).
\Find the pressure when altitude is
m.
Substitute
in the equation
.

The Pressure is
kpa when altitude is
m.
(a) The pressure is
kpa at an altitude of
.
(b) The Pressure is
kpa when altitude is
m.