Two Body Problem MCQ
Test your knowledge with important Two Body Problem MCQ and their applications. These MCQs are beneficial for competitive exams too. Explore 30+ more Two Body Problem MCQs on Bissoy. Bissoy App
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In the following equation, what are orbital constants? r = .
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For two-body problems, satellite motion is represented as __________ motion.
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What is the eccentricity of an orbit if tangential and radial velocity are 9.08 km/s and 2.01 km/s respectively. Specific angular momentum is 63,585 km2/s. Standard gravitational parameter is 398,600 km3/s2.
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What is the specific angular momentum of an elliptical orbit, if the flight path angle of the satellite in orbit at an instant is 15°? The satellite is travelling at a velocity of 10.7 km/s at the same instant and is parked at an altitude of 7048 km measured from earth’s center.
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How long does it take for a satellite to travel between perigee and apogee? Apogee and perigee altitude from surface of the earth is 900 km and 400 km respectively. Earth’s radius and standard gravitational parameter is 6378 km and 398,600 km3/s2 respectively.
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What is the velocity of a satellite orbiting around moon in a circular orbit of altitude 100 km from moon’s surface. Given, standard gravitational parameter of moon is 4903 km3/s2 and radius of moon is 1738 km.
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What is the area swept by a satellite in an elliptical orbit around earth at t = T/5, where T is the time period of the orbit? Given, semi-major axis and semi-minor axis of the orbit are 9,000 km and 4,000 km respectively.
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The two-body problem assumes both bodies as point masses.