Question 1:
Compare and contrast geostationary and non-geostationary satellites.
Answer:

Compare and contrast geostationary and non-geostationary satellites.
Answer:

Question 2:
What factors determine the linear speed of satellites orbiting the Earth?
Answer:
Linear speed of satellite, v=√GMr
As GM is constant, linear speed of the satellite only depends on the radius of its orbit. If a satellite is at a height, h above the surface of the Earth, r = R + h (R = radius of the Earth).
What factors determine the linear speed of satellites orbiting the Earth?
Answer:
Linear speed of satellite, v=√GMr
As GM is constant, linear speed of the satellite only depends on the radius of its orbit. If a satellite is at a height, h above the surface of the Earth, r = R + h (R = radius of the Earth).
Question 3:
State two factors which infl uence the value of escape velocity from a planet.
Answer:
Escape velocity, v=√2GMr
Thus, the two factors which influence the value of escape velocity from a planet are:
1. Mass of the planet
2. Distance from the centre of the planet
State two factors which infl uence the value of escape velocity from a planet.
Answer:
Escape velocity, v=√2GMr
Thus, the two factors which influence the value of escape velocity from a planet are:
1. Mass of the planet
2. Distance from the centre of the planet
Question 4:
Discuss whether escape velocity from the Earth for spacecraft X of mass 1 500 kg is different from spacecraft Y of mass 2 000 kg.
Answer:
No, because the escape velocity, v of an object does not depend on the mass of the object.
Discuss whether escape velocity from the Earth for spacecraft X of mass 1 500 kg is different from spacecraft Y of mass 2 000 kg.
Answer:
No, because the escape velocity, v of an object does not depend on the mass of the object.
Question 5:
Proba-1 satellite orbits the Earth at a height of 700 km. What is the linear speed of this satellite?
[G = 6.67 × 10–11 N m2 kg–2, mass of the Earth = 5.97 × 1024 kg, radius of the Earth = 6.37 × 106 m]
Answer:
h=700 km=7.0×105 mG=6.67×10−11Nm2 kg−2ME=5.97×1024 kgR=6.37×106 mv=?r=R+h=(6.37×106)+(7.0×105)=7.07×106 m
v=√GMR+h=√(6.67×10−11×(5.97×1024)7.07×106v=7504.83 ms−1
Proba-1 satellite orbits the Earth at a height of 700 km. What is the linear speed of this satellite?
[G = 6.67 × 10–11 N m2 kg–2, mass of the Earth = 5.97 × 1024 kg, radius of the Earth = 6.37 × 106 m]
Answer:
h=700 km=7.0×105 mG=6.67×10−11Nm2 kg−2ME=5.97×1024 kgR=6.37×106 mv=?r=R+h=(6.37×106)+(7.0×105)=7.07×106 m
v=√GMR+h=√(6.67×10−11×(5.97×1024)7.07×106v=7504.83 ms−1