Gareth56 Posted January 20, 2009 Share Posted January 20, 2009 In College Physics 7th Ed by Serway it states that the tangential speed of the surface of the Earth at the equator is 1700m/s!! Is this correct? I thought it was more like 465m/s. Link to comment Share on other sites More sharing options...
D H Posted January 20, 2009 Share Posted January 20, 2009 Can you give a quote from that book in context? You are correct: 2*pi/sidereal day * 6378 km = 465 m/s. Link to comment Share on other sites More sharing options...
timo Posted January 20, 2009 Share Posted January 20, 2009 [math] v = \frac{2 \pi r}{24 \text{ h}} \approx \frac{6 \cdot 6 \cdot 10^3 \text{ km}}{24\text{ h}} = \frac{36\cdot 10^3}{24} \frac{\text{km}}{\text{h}} = 1500 \frac{\text{km}}{\text{h}}.[/math]. So if "tangential speed" is defined the way I assumed, then it seems you are right. However, seeing that I did some approximations it is well possible that the actual value would be ~1700 km/h. In that case the college book might have screwed up the units (or you misread them). Link to comment Share on other sites More sharing options...
D H Posted January 20, 2009 Share Posted January 20, 2009 However, seeing that I did some approximations it is well possible that the actual value would be ~1700 km/h. In that case the college book might have screwed up the units (or you misread them). Good catch. Gareth56, double-check the units in the text. Is it kilometers per hour or meters per second? 2*pi/sidereal day * 6378 km = 1674 km/hr. Note well: It is 2*pi/sidereal day, not 2*pi/24 hours. There is a slight difference, probably important only to the truly pedantic. A sidereal day is 23.9344696 hours long. Link to comment Share on other sites More sharing options...
Gareth56 Posted January 21, 2009 Author Share Posted January 21, 2009 Here is the exact quote from the book:- "Why is the launch area for the European Space Agency in South America and not in Europe? Explanation:- Satellites are boosted into orbit on top of rockets, which provide the large tangential speed necessary to achieve orbit. Due to its rotation, the surface of Earth is already traveling toward the east at a tangential speed of nearly 1700 m/s at the equator. This tangential speed is steadily reduced further north, because the distance to the axis of rotation is decreasing. It finally goes to zero at the North Pole. Launching eastward from the equator gives the satellite a starting initial tangential speed of 1700 m/s, whereas a European launch provides roughly half that speed (depending on the exact latitude)." Link to comment Share on other sites More sharing options...
swansont Posted January 21, 2009 Share Posted January 21, 2009 I'm guessing it's the unit mistake, and should be km/hr. You could contact the publisher and point that out. They might have an errata page online. Is there a URL given in the book? Link to comment Share on other sites More sharing options...
Gareth56 Posted January 21, 2009 Author Share Posted January 21, 2009 I understand there's now an 8th edition so hopefully the proof reader spotted the typo. Link to comment Share on other sites More sharing options...
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