To circle Earth in low orbit, a satellite must have a speed of about 2.8 x 104 km/h. Suppose that two such satellites orbit Earth in opposite directions. (a) What is their relative speed as they pass, according to the classical Galilean velocity transformation equation? (b) VWhat fractional error do you make in (a) by not using the (correct) relativistic transformation equation? (a) Number i Units (b) Number i Units

Classical Dynamics of Particles and Systems
5th Edition
ISBN:9780534408961
Author:Stephen T. Thornton, Jerry B. Marion
Publisher:Stephen T. Thornton, Jerry B. Marion
Chapter14: Special Theory Of Relativity
Section: Chapter Questions
Problem 14.9P
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To circle Earth in low orbit, a satellite must have a speed of about 2.8 × 104 km/h. Suppose that two such satellites orbit Earth in
opposite directions. (a) What is their relative speed as they pass, according to the classical Galilean velocity transformation
equation? (b) What fractional error do you make in (a) by not using the (correct) relativistic transformation equation?
(a) Number
i
Units
(b) Number
i
Units
<>
Transcribed Image Text:To circle Earth in low orbit, a satellite must have a speed of about 2.8 × 104 km/h. Suppose that two such satellites orbit Earth in opposite directions. (a) What is their relative speed as they pass, according to the classical Galilean velocity transformation equation? (b) What fractional error do you make in (a) by not using the (correct) relativistic transformation equation? (a) Number i Units (b) Number i Units <>
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