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St. John's University *

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1060

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Physics

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Dec 6, 2023

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ASTR 1403 HOMEWORK - SET 4 Due 11/2/23 GEOSTATIONARY ORBITS - LOCATION, LOCATION, LOCATION A satellite is geostationary if it appears fixed in the sky as seen by an observer on Earth. Geostationary satellites are very useful for communication and a lot of them are in use. Access to geostationary orbit is regulated by international treaty and a spot in geostationary orbit is probably the most desirable “unreal estate” | can think of. What goes into making an orbit geostationary? Kepler’'s and Newton’s laws, and location, location, location. We will determine how this works in these exercises. Kepler’s first law in this context states that the orbit of a satellite is an ellipse with the center of the Earth at one focus. Kepler’s second law states that the line joining the satellite and the center of the Earth sweeps out equal areas in equal intervals of time. Kepler’s third law (in Newtonian form) relates the orbital period of the satellite to the semi-major axis of the orbit and the mass of the Earth. In order to appear geostationary, a satellite must have a circular orbit, the satellite must orbit in the Earth’s equatorial plane, it must have the correct orbital period, and it must go around the Earth the correct way. We will explore each of these requirements below. 1 For this question assume the satellite’s orbit is circular and lies in the Earth’s equatorial plane. For parts (b) and (c) assume the satellite goes around the correct way. a) What is the required orbital period for a geostationary satellite? In what direction must the satellite orbit? b) What would an earthbound observer see if the orbital period of the satellite was too short? C) What would an earthbound observer see if the orbital period of the satellite was too long? d) What would an earthbound observer see if the satellite went around the Earth the wrong way? 2. What does the semi-major axis of the orbit need to be? What happens if the semi-major axis is too small? What happens if it is too large? What is the ratio of the semi-major axis of a geostationary satellite to the radius of Earth? 3. Suppose the satellite has the correct orbital period, goes around the correct way, and has a circular orbit. However, its orbit is inclined with respect to the Earth’s equatorial plane be a small amount. What would an earthbound observer see the satellite do? 4. Suppose the satellite has the correct orbital period, goes around the correct way;, and orbits in Earth’s equatorial plane. However, the orbit is not circular. The orbit has a small eccentricity. What would an earthbound observer see the satellite do?
The arch villains in a dastardly, supersecret global conspiracy of evil geniuses devoted to complete and total world domination are insanely jealous of Santa Claus. Santa can deliver toys to all the good, little girls and boys in just one night using only a sleigh and flying reindeer. And he knows if you have been bad or good! The dastardly villains have never been able to get that kind of information from their extensive network of spies and informants. These evil geniuses want to put a geostationary satellite directly over the north pole so they can steal Santa’s secrets. You are the only technical expert advising them on the project. Can they do it? Be careful with your answer. Supervillains do not like the word no. The evil geniuses have placed their satellite in their chosen spot. Describe the space motion of their satellite. What will happen to it? What should Santa do? Rotation Period of Earth (sidereal) = 86,164 s Earth Day = 24 hours = 86,400 s Earth: GM = 398,600 km”3/s/2 Earth Radius = 6371 km The planet Mars is orbited by two small moons, Phobos and Deimos. Both moons have circular orbits. Use Kepler’s third law in Newtonian form to compute the mass of Mars from the orbital dats for the two moons and Newton’s constant. a) Phobos: a=9377 km; P =0.3189 days b) Deimos: a = 23,460 km; P =1.2624 days Newton’s Constant G = 6.673 x 107(-11) m”3/kg s"2 Marvin the Martian thinks geostationary satellites are really cool and he wants one for Mars. The sidereal rotation period of Marsis P = 1.026 days = 88,646 s. Assume that Marvin’s satellite has a circular orbit in the equatorial plane of Mars and that it goes around Mars the correct way. a) What orbital radius does Marvin need for his Mars-stationary satellite? How many Mars radii is this? The radius of Marsis R = 3390 km. b) Marvin observes the motion of Phobos, Deimos, and his new satellite in the Martian sky. Describe the motion he sees. Where do the objects rise and set? How do they move in the Martian sky. Assume that North, South, East and West are defined on Mars by the rotation of Mars the same way they are defined by the rotation of Earth on Earth. (] 3 ~tt 3 2 e G= Le7F3»l0 M [y < = ;—" . 2 H(Eerdl) = SaF x10 h 2 3 T « l L:a 'H\ Dfii/ - Zk{L,yt = &6ILIOOf
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