<span>r = GM/v^2
r is the distance of the satellite from the center of Earth in meters
G is newtons constant, 6.67428 x 10^-11
M is the mass of Earth, 5.9742 x 10^24
v is the orbital speed, which we know is 5,000 m/s
r = 6.67428 x 10^-11 x 5.9742 x 10^24/5,000^2
r = 8,137,445 meters from the center of the Earth
and : 8,137,445 - 6,378,100 = 1,749,345 meters from the surface of the Earth
Now that we know the distance we can calculate the orbital period.
Time = Distance/speed
distance is the circumference of the orbit, 2Ď€ x 8,137,445 = 51,129,074 meters
Time = (51,129,074)/5,000
Time = 10,225 seconds = 2.84 hours
so, orbital period is 2.84 hrs</span>
i would choose steel because the steel used for normal construction have several hundred Mega Pascal strength. one of the special feature of steel is its ductility. it is the deformation capability before the final breakage.
The frequency of rotation of an object in order to achieve required centripetal or radial acceleration, can be found out by using the following formula: