0:00
Hello.
00:01
First we can solve part a of this question.
00:04
In this question, the space station is in stable orbit around the earth.
00:08
Therefore we can write fc is equal to fg, where fc is the centripetal force and fg is the gravitational force accepted by the earth on the space station.
00:18
Now fc can be written as m v squared divided by r, where m is the mass of the space station, v is the orbital speed of the space station and r is the radius of orbit of the space station.
00:30
It can be written as equal to fg can be written as g m divided by r square.
00:38
Here g is gravitational constant and capital m is the mass of the earth.
00:43
Simplifying this equation, the equation for orbital speed can be written as v is equal to root of gm divided by r.
00:53
Here g and m are constants, therefore the orbital speed v is inversely proportional to the square of.
01:00
Root of r, where r is the radius of orbit of the space station.
01:05
Therefore we can conclude that the orbital speed v does not depend upon the mass m of the space station.
01:20
Now in part b we can write r is equal to capital r plus h.
01:28
Here r is the radius of the earth and h is the height of the space station with respect to the earth's surface.
01:34
The value of r is equal to 6 ,000 370 km, it can be written as equal to 6 ,370 into 10 raised to 3 meter.
01:47
H is given to be equal to 415 km, it can be written as equal to 415 into 10 raise to 3 meter.
01:58
We can substitute the values here so it equals 6 ,370 into 10 raised to 3 meter plus 415 into 10 raised to 3 meter plus 415 into 10 raised to 3 meter...