A spaceship with m = 1.00 ✕ 104 kg is in a circular orbit around the Earth, h = 800 km above its surface. The ship's captain fires the engines in a direction tangent to the orbit, and the spaceship assumes an elliptical orbit around the Earth with an apogee of d = 3.00 ✕ 104 km, measured from the Earth's center. How much energy (in J) must be used from the fuel to achieve this orbit? (Assume that all the fuel energy goes into increasing the orbital energy and that the perigee distance is equal to the initial radius.) 14. [0/1 Points]DETAILSPREVIOUS ANSWERSSERPSE10 13.A.OP.036.MY NOTESASK YOUR TEACHERPRACTICE ANOTHERA spaceship with m = 1.00 x 104 kg is in a circular orbit around the Earth, h = 800 km above its surface. The ship's captain fires the engines in a direction tangent to the orbit, and the spaceship assumes an elliptical orbit around the Earth with an apogee ofd = 3.00 x 1o4 km, measured from the Earth's center. How much energy (in J) must be used from the fuel to achieve this orbit? (Assume that all the fuel energy goes into increasing the orbital energy, and that the perigee distance is equal to the initial radius.)Calculate the initial and final energies of the orbit. Assume the perigee distance is the initial circular orbital distance. Find the change in energy. JNeed Help?Read ItSubmit Answer

Given: Mass of spaceship, m = 1 X104 kg Height of spaceship = 800 km Apogee , d = 3 X 104 km Mass of…

Answered: A spaceship with m = 1.00 ✕ 104 kg is…

College Physics

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ISBN:9781305952300

Author:Raymond A. Serway, Chris Vuille

Publisher:Raymond A. Serway, Chris Vuille

Chapter1: Units, Trigonometry. And Vectors

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A spaceship with m = 1.00 ✕ 10⁴ kg is in a circular orbit around the Earth, h = 800 km above its surface. The ship's captain fires the engines in a direction tangent to the orbit, and the spaceship assumes an elliptical orbit around the Earth with an apogee of d = 3.00 ✕ 10⁴ km, measured from the Earth's center. How much energy (in J) must be used from the fuel to achieve this orbit? (Assume that all the fuel energy goes into increasing the orbital energy and that the perigee distance is equal to the initial radius.)

14. [0/1 Points]
DETAILS
PREVIOUS ANSWERS
SERPSE10 13.A.OP.036.
MY NOTES
ASK YOUR TEACHER
PRACTICE ANOTHER
A spaceship with m = 1.00 x 104 kg is in a circular orbit around the Earth, h = 800 km above its surface. The ship's captain fires the engines in a direction tangent to the orbit, and the spaceship assumes an elliptical orbit around the Earth with an apogee of
d = 3.00 x 1o4 km, measured from the Earth's center. How much energy (in J) must be used from the fuel to achieve this orbit? (Assume that all the fuel energy goes into increasing the orbital energy, and that the perigee distance is equal to the initial radius.)
Calculate the initial and final energies of the orbit. Assume the perigee distance is the initial circular orbital distance. Find the change in energy. J
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