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For the next question, consider that for any orbiting system, the total system mass (TSM) = a³/P2, where a is the length of the semi-major axis (how far apart the orbiting object gets from the center of the orbit) in A.U., and Pis the period of the orbit in years. Q-22: Now assume that the average separation between the two components is 0.3 A.U., and convert your answer for the period of this system in to a fraction of a year by dividing. What is the approximate combined mass of the two components? O a) 3 b) 21 O c) 39 d) 42 e) 70 Of) 130 Og) 200

For the next question, consider that for any orbiting system, the total system mass (TSM) = a³/P2, where a is the length of the semi-major axis (how far apart the orbiting object gets from the center of the orbit) in A.U., and Pis the period of the orbit in years. Q-22: Now assume that the average separation between the two components is 0.3 A.U., and convert your answer for the period of this system in to a fraction of a year by dividing. What is the approximate combined mass of the two components? O a) 3 b) 21 O c) 39 d) 42 e) 70 Of) 130 Og) 200

Applications and Investigations in Earth Science (9th Edition)
Applications and Investigations in Earth Science (9th Edition)
9th Edition
ISBN:9780134746241
Author:Edward J. Tarbuck, Frederick K. Lutgens, Dennis G. Tasa
Publisher:Edward J. Tarbuck, Frederick K. Lutgens, Dennis G. Tasa
Chapter1: The Study Of Minerals
Section: Chapter Questions
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For the next question, consider that for any orbiting system, the total system mass (TSM) = a³/P2, where a is the length of the semi-major axis (how far apart the orbiting object gets from the center of the orbit) in A.U., and P is the period of the orbit in years. Q-22: Now assume that the average separation between the two components is 0.3 A.U., and convert your answer for the period of this system in to a fraction of a year by dividing. What is the approximate combined mass of the two components? a) 3 b) 21 c) 39 d) 42 e) 70 Of) 130 g) 200
Transcribed Image Text:For the next question, consider that for any orbiting system, the total system mass (TSM) = a³/P2, where a is the length of the semi-major axis (how far apart the orbiting object gets from the center of the orbit) in A.U., and P is the period of the orbit in years. Q-22: Now assume that the average separation between the two components is 0.3 A.U., and convert your answer for the period of this system in to a fraction of a year by dividing. What is the approximate combined mass of the two components? a) 3 b) 21 c) 39 d) 42 e) 70 Of) 130 g) 200
Q-23: In what units would this mass be? a) Pounds Ob) Tons Oc) Kilograms о d) Metric tons e) Earth masses Of) Solar masses Og) Moon masses
Transcribed Image Text:Q-23: In what units would this mass be? a) Pounds Ob) Tons Oc) Kilograms о d) Metric tons e) Earth masses Of) Solar masses Og) Moon masses
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