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Satellites. Why do objects move in a circle? 0eo&feature=related 0eo&feature=related.

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Presentation on theme: "Satellites. Why do objects move in a circle? 0eo&feature=related 0eo&feature=related."— Presentation transcript:

1 Satellites

2 Why do objects move in a circle? 0eo&feature=related 0eo&feature=related

3 Why doesn’t the moon fall down? It does. 8&feature=related 8&feature=related

4 What is a satellite? Technically, anything that is in orbit around Earth is technically a satellite, but the term "satellite" is typically used to describe a useful object placed in orbit purposely to perform some specific mission or task. We commonly hear about weather satellites, communication satellites and scientific satellites.

5 Whose Satellite Was the First to Orbit Earth? The Soviet Sputnik satellite was the first to orbit Earth, launched on October 4, 1957. It weighed 184 pounds and was 23” in diameter.

6 What happened to it? After 92 days, gravity took over and Sputnik burned in Earth's atmosphere. Thirty days after the Sputnik launch, the dog Laika orbited in a half-ton Sputnik satellite with an air supply for the dog. It burned in the atmosphere in April 1958.

7 Progress since then… ISS Video best-time-lapsed-videos-of-earth-from-space- yet/ best-time-lapsed-videos-of-earth-from-space- yet/

8 How Do You Put Something In Orbit? If the Earth were flat like some people used to believe, no matter how fast you threw something out horizontally, it would hit the ground. The faster you threw it, the farther away along the ground it would hit. Plus - all of the balls will hit the ground at the same time.

9 But the Earth is not flat! As something falls "straight" toward the center of the Earth, it has to curve around with the Earth.


11 Throw an object fast enough that its “fall” matches the curvature of the Earth. The Earth’s curvature is such that it “drops” about 5 meters every 8,000 m. So what speed would it have to go to orbit the Earth at the surface? 8 km/s!

12 The only force on a satellite is the force of gravity. That’s the force pulling it in to the center.

13 Launch Space shuttle Atlantis final launch: NASA video of last take-off Pgg Pgg Mars exploration rover

14 Let’s use equations to check how fast an object near the Earth’s surface is orbiting? Fg = Fc Fg = mv 2 / r m g = m v 2 / r g = v 2 / r v 2 = g r If r = 6.38 x 10 6 m, what is v?

15 The orbital velocity is v 2 = ( 9.8 m/s ) ( 6.38 x 10 6 m ) = 6.25 x 10 7 (m/s) 2 v = 7.9 x 10 3 m/s That’s 17 000 mi/h!

16 What about the period? How long does it take to make one orbit? v = d / T T = d / v T = 2π r / v T = 2 ( 3.14 ) ( 6.38 x 10 6 m ) / ( 7.9 x 10 3 m/s ) T = 5074 s [ 1 min/60 s ] = 84 min

17 The Space Shuttle is an excellent example of a satellite in a low-Earth orbit. The Space Shuttle orbits about 100 km to 200 km above Earth's surface. Earth's radius is about 6 000 km so this is an increase of only about 2% or 3%. That means the force of gravity is only about 4% to 6% less than at Earth's surface.

18 Low Earth Orbit Imagine yourself in an elevator when the cable breaks! The only force on you is gravity!

19 The Physical Aspect Bodily fluids are redistributed, with less in the lower extremities, and more in the upper body. Without the pulls of normal gravity, blood doesn't flow downhill, but pools in the extremities including the face, hands and feet, causing a puffy appearance. And without that downward pressure, height increases. Body mass often decreases with a loss of muscular tissue from nitrogen depletion; the veins and arteries of the legs become weaker, anemia occurs, accompanied by a reduction in blood count. Astronauts report an overall feeling of weakness and loss of balance upon return to Earth, though recovery is nearly complete after a week.

20 Types of Satellites

21 Types of Orbits Polar Orbits This orbit allows the satellite to observe the entire Earth's surface as it rotates beneath it. Most desired orbits are between 700 and 800 km altitude with orbit periods between 98 and 102 minutes.

22 Uses of Polar Orbiting Satellites This orbit provides global daily coverage of the Earth with higher resolution than geostationary orbit. Even though satellites do not pass directly over the poles they come close enough that their instruments can scan over the polar region, providing truly global coverage.

23 Geosynchronous Satellites Orbit around the Earth at the same speed that the Earth rotates. What’s its period? 24 hours If they stay over the same place, they are called geostationary. Where do they orbit? Over the equator. Because of this, it appears to remain over a fixed point on the Earth's surface.

24 Uses of Geosynchronous Satellites Perfect for communications satellites because always in view of the ground station providing continuous TV and telecommunications services to customers. Also ideal for making uninterrupted observations of the weather or environmental conditions in a given area.

25 Definitions: Geosynchronous- same period as Earth Geostationary – orbits over the same location on Earth Asynchronous – not once a day, like the space station.

26 What is the orbital radius of a geosynchronous satellite? Fg = Fc Fg = mv 2 / r GM E M S /r 2 = M S v 2 / r GM E /r 2 = (2πr/T) 2 / r GM E /r 2 = (2πr) 2 / T 2 r GM E /r 2 = 4π 2 r 2 / T 2 r

27 Move r 2 to top GM E = 4π 2 r 2 r 2 / T 2 r GM E = 4π 2 r 3 / T 2 Solving for r: r 3 = GM E T 2 / 4π 2 This means that for a fixed period – like 24 hr – there is only ONE radius that will work!!

28 r 3 = (6.67 x 10 -11 )(6 x 10 24 kg)(86,400s) 2 /4 π 2 r 3 = 7.54 x 10 22 m 3 r = 4.2 x 10 7 m If we subtract off the radius of the Earth, which is 6.38 x 10 6 m (or 6380 km), then The orbital radius is 36,000 km above earth, or 6 r E (6 times Earth’s radius).

29 What’s the velocity of a geosynchronous satellite? Fg = Fc Fg = mv 2 / r GM E M S /r 2 = M S v 2 / r GM E /r 2 = v 2 / r GM E /r = v 2 v= square root of (GM E /r) V = 3070 m/s

30 So all the geosynchronous satellites orbit at this radius!

31 Geosynchronous orbits are 1/10 the distance to the moon!

32 Space Junk at Tipping Point Q&feature=fvsr Q&feature=fvsr Debris – green dots 4s 4s

33 What happens when satellites plunge back toward Earth? This happened on Sept. 22, 2011. Watch Out! NASA UARS satellite to hit Earth... Anywhere! (Upper Atmosphere Research Satellite) dM dM mNATU&feature=related mNATU&feature=related

34 Comparing velocity, radius and period: Radius r Period T Velocity v Surface/ LEO6.38 x 10 6 m 83 min.8 km/s Geostationary4.23 x 10 7 m 24 hr.3 km/s Moon3.84 x 10 8 m 27.3 days1 km/s

35 Does this make sense? Doesn’t v = 2πr/T? Then doesn’t that mean that as r ↑, v ↑? But v depends on T, so to eliminate v: Fc = Fg ⇒ m S v 2 /r = Gm S m E / r 2 ⇒ v = √Gm E /r v 2 = Gm E /r = 4π 2 r 2 /T 2 r 3 /T 2 = Gm/4π 2 = constant r 3 ∝ T 2 So as r increases, T increases.

36 Summary - 2 ways to find velocity: V = 2πr / T V = √ (GME/r) (This means square root!) Where r is the orbital radius, not the height above the surface.

37 Problem Solving What is the speed of a space shuttle in a circular orbit 1000km above Earth’s surface? The mass of Earth is 6 x 10 24 kg and the radius of Earth is 6.38 x 10 6 m. G = 6.67 x 10 -11.

38 Solution R = 7.38 x 10 6 m Fc = Fg V 2 = GMe/R V = 7.35 x 10 3 m/s or 16,500 mph

39 NASA GOES - P Mission Overview PC94&feature=related PC94&feature=related Cup of coffee 3zg&feature=related 3zg&feature=related Going to the bathroom UPSo&feature=related UPSo&feature=related

40 Space Junk Video 4 min. satellite-technology-orbit-and-orbital-debris- video.htm satellite-technology-orbit-and-orbital-debris- video.htm

41 Real Time Satellite Tracking Click and drag applet

42 Tracking ISS Another ISS tracking site. index.html index.html

43 Satellite Tracking Position of ISS and other satellites rack3d.html rack3d.html

44 History of ISS ion_worldbook.html ion_worldbook.html

45 Attitudes of ISS Adjusting the angle for solar panels. ttitude.html ttitude.html

46 Interactive Reference Guide Videos of how the crew eats, sleeps and exercises.

47 Upcoming Launches edule.html edule.html

48 NASA in motion Link to NASA Drawing Video

49 Cup of Joe Link to Cup of Joe Video

50 Atlantis leaves ISS Link to Undocking Video

51 Takeoff and Landing of Discovery 2bDb4 2bDb4

52 Apollo Guys – Co Ops Link Apollo Guys (Apologize) Watching on the screen Saturn V lifts off the ground After many sims, Flight control has got it down You say that its not easy, but Astronauts are all moonbound and wait Were watching them on TV Walking on the lunar ground and say We did it Apollo Guys! Link Apollo Guys (Apologize)

53 How GPS Works

54 The dashed lines show the actual intersection point, and the gray bands indicate the area of uncertainty.

55 The solid lines indicate where the GPS receiver "thinks" the spheres are located. Because of errors in the receiver's internal clock, these spheres do not intersect at one point. Three spheres are necessary to find position in two dimensions, four are needed in three dimensions.

56 Problem Solving #1 A satellite over Jupiter is placed 6 x 10 5 m above surface, given mass of Jupiter, find v. Mass of Jupiter = 2 x 10 27 kg, Radius of Jupiter = 71,492 kilometers So r = radius of Jupiter + height over surface r = 7.2 x 10 7 m V 2 = GM J /r v 2 = 1.76 x 10 9 m/s v = 4.195 x 10 4 m/s

57 Problem Solving #2 A satellite wishes to orbit the earth at a height of 100 km (approximately 60 miles) above the surface of the earth. Determine the speed, acceleration and orbital period of the satellite. (Given: M earth = 5.98 x 10 24 kg, R earth = 6.37 x 10 6 m) Speed = = 7.85 x 10 3 m/s Acceleration = a = 9.53 m/s 2 Orbital period = T = 5176 s = 1.44 hrs

58 #3 One of Saturn's moons is named Mimas. The mean orbital distance of Mimas is 1.87 x 10 8 m. The mean orbital period of Mimas is approximately 23 hours (8.28x10 4 s). Use this information to estimate a mass for the planet Saturn. Using the T and R values given, the T 2 / R 3 ratio is 1.05 x 10 -15. This ratio is equal to 4*pi 2 / G * M central. Mass of Saturn can be found to be 5.64 x 10 26 kg.

59 #4 Satellites circling unknown planet. Sat1 has v1 = 1.7 x 10 4 m/s, and r = 5.25 x 10 6 m. Sat2 has r = 8.6 x 10 6 m. Find v for Sat2. V 2 = GM PLANET /r So M PLANET G = constant = v 2 r V 1 2 r 1 = v 2 2 r 2 V 2 = 1.33 x 10 4 m/s

60 Which of following statements is accurate regarding man-made satellites? A. It is possible to have a satellite traveling at either a high speed or at a low speed in a given circular orbit. B. Only circular orbits (and not elliptical ones) are possible for artificial satellites. C. A satellite in a large diameter circular orbit will always have a longer period of revolution about the earth than will a satellite in a smaller circular orbit. D. The velocity required to keep a satellite in a given orbit depends on the mass of the satellite.


62 Next Genertion Car Navigation

63 Practice Questions Giancoli ultiple1/deluxe-content.html ultiple1/deluxe-content.html

64 Satellites orbiting earth 2gc 2gc

65 Launching Satellites 2Ga0 2Ga0


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