Fig Explain how the lift force L maintains the aeroplane flying in a horizontal circle [2]

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Transcription:

1 (a) Fig. 2.1 shows an aeroplane flying in a horizontal circle at constant speed. The weight of the aeroplane is W and L is the lift force acting at right angles to the wings. L centre of circle aeroplane W Fig. 2.1 Explain how the lift force L maintains the aeroplane flying in a horizontal circle.... [2] The aeroplane of mass 1.2 10 5 kg is flying in a horizontal circle of radius 2.0 km. The centripetal force acting on the aeroplane is 1.8 10 6 N. Calculate the speed of the aeroplane. speed =... m s 1 [2] (b) Fig. 2.2 shows a satellite orbiting the Earth at a constant speed v. The radius of the orbit is r. v satellite r Earth Fig. 2.2

Show that the orbital period T of the satellite is given by the equation T 2 = 4π2 r 3 GM where M is the mass of the Earth and G is the gravitational constant. (c) The satellites used in television communication systems are usually placed in geostationary orbits. In your answer, you should use appropriate technical words spelled correctly. [3] State two features of geostationary orbits. 1.... 2....... [2] Calculate the radius of orbit of a geostationary satellite. The mass of the Earth is 6.0 10 24 kg. radius =... m [3] [Total: 12]

2 A satellite orbits the Earth in a circular path 800 km above the Earth s surface. At the orbit of the satellite the gravitational field strength is 7.7 N kg 1. The radius of the Earth is 6400 km. (a) Calculate the orbital speed of the satellite orbital speed =... m s 1 [3] the period of the orbit of the satellite. period =... s [2]

(b) The orbit of the satellite passes over the Earth s poles. Show that the satellite makes about 14 orbits around the Earth in 24 hours. [1] The cameras on board the satellite continually photograph a strip of the Earth s surface, of width 3000 km, directly below the satellite. Determine, with an appropriate calculation, whether the satellite can photograph the whole of the Earth s surface in 24 hours. State your conclusion.... [3] (c) Suggest a practical use of such a satellite....... [1] [Total: 10]

3 (a) State, in words, Newton s law of gravitation.......... [1] (b) Fig. 3.1 shows the circular orbits of two of Jupiter s moons: Adrastea, A, and Megaclite, M. A Jupiter M not to scale Fig. 3.1 Use the following data in the calculations below. orbital radius of A = 1.3 10 8 m orbital period of A = 7.2 hours gravitational field strength at orbit of A = 7.5 N kg 1 orbital radius of M = 2.4 10 10 m Calculate the mass of Jupiter mass =... kg [3]

the gravitational field strength at the orbit of M (iii) the orbital period of M. gravitational field strength =... N kg 1 [2] orbital period =... hours [3] [Total: 9]

4 (a) State the name given to satellites that orbit the Earth, with a period of 1 day, above the equator. You should use the appropriate technical term spelled correctly.... [1] Explain why these satellites orbit above the equator.... [1] (iii) For companies who provide a satellite TV service, suggest the main advantage of using this type of satellite.... [1] (iv) The mass of the Earth is 6.0 10 24 kg. Show that the radius of the orbit of a satellite with an orbital period of 1 day is about 4 10 7 m. [3] (b) State Kepler s third law.... [1] The Moon orbits the Earth with a period of 27.3 days. Use the information given in (a)(iv) to calculate the following ratio: distance of the Moon from the Earth s centre distance of the satellite from the Earth s centre r atio =... [2] [Total: 9]

5 (a) State, in terms of force, the conditions necessary for an object to move in a circular path at constant speed.... [1] Explain why this object is accelerating. State the direction of the acceleration.... [2] (b) A satellite moves in a circular orbit around the Earth at a constant speed of 3700 m s 1. The mass M of the Earth is 6.0 10 24 kg. Calculate the radius of this orbit. radius =... m [4] (c) In order to move the satellite in (b) into a new smaller orbit, a decelerating force is applied for a brief period of time. Suggest how the decelerating force could be applied.... [1] The radius of this new orbit is 2.0 10 7 m. Calculate the speed of the satellite in this orbit. speed =... m s 1 [2] [Total: 10]