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Satellite Motion

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Q. A satellite is in a circular orbit around the Earth. If it moves to a higher orbit, what happens to its potential energy?
  • A. It increases.
  • B. It decreases.
  • C. It remains constant.
  • D. It becomes zero.
Q. A satellite is in a circular orbit around the Earth. If its speed is doubled, what will happen to its orbital radius?
  • A. It will remain the same.
  • B. It will double.
  • C. It will increase by a factor of four.
  • D. It will decrease by a factor of four.
Q. A satellite is in a circular orbit around the Earth. If its speed is doubled, what happens to the radius of its orbit?
  • A. It remains the same
  • B. It doubles
  • C. It increases by a factor of four
  • D. It decreases by a factor of four
Q. A satellite is in a circular orbit around the Earth. If its speed is increased, what will happen to its orbit?
  • A. It will remain circular
  • B. It will become elliptical
  • C. It will crash into the Earth
  • D. It will escape Earth's gravity
Q. A satellite is in a circular orbit around the Earth. If the radius of the orbit is halved, what happens to the gravitational force acting on the satellite?
  • A. It remains the same
  • B. It doubles
  • C. It quadruples
  • D. It decreases by half
Q. A satellite is in a circular orbit around the Earth. If the satellite's speed is increased, what will happen to its orbit?
  • A. It will remain circular
  • B. It will become elliptical
  • C. It will crash into the Earth
  • D. It will escape Earth's gravity
Q. A satellite is in a circular orbit at a height of 300 km above the Earth's surface. What is the approximate speed of the satellite?
  • A. 7.9 km/s
  • B. 5.0 km/s
  • C. 10.0 km/s
  • D. 3.5 km/s
Q. A satellite is in a polar orbit. What is the significance of this orbit?
  • A. It allows the satellite to cover the entire surface of the Earth.
  • B. It is the fastest orbit available.
  • C. It is used only for communication satellites.
  • D. It is the most stable orbit.
Q. A satellite orbits the Earth at a height of 500 km. What is the approximate gravitational acceleration experienced by the satellite?
  • A. 9.8 m/s²
  • B. 7.9 m/s²
  • C. 8.7 m/s²
  • D. 6.0 m/s²
Q. For a satellite in a circular orbit, which of the following is true about its kinetic and potential energy?
  • A. K.E. = P.E.
  • B. K.E. > P.E.
  • C. K.E. < P.E.
  • D. K.E. = 0
Q. For a satellite in a low Earth orbit, what is the approximate altitude range? (2000)
  • A. 200-2000 km
  • B. 500-10000 km
  • C. 1000-20000 km
  • D. 30000-40000 km
Q. For a satellite in a stable orbit, what must be true about the centripetal force and gravitational force?
  • A. Centripetal force is greater than gravitational force
  • B. Centripetal force is less than gravitational force
  • C. Centripetal force equals gravitational force
  • D. Centripetal force is independent of gravitational force
Q. If a satellite is in a geostationary orbit, what is its orbital period?
  • A. 24 hours
  • B. 12 hours
  • C. 6 hours
  • D. 1 hour
Q. If a satellite is in a stable orbit, what can be said about the net force acting on it?
  • A. It is zero
  • B. It is equal to the gravitational force
  • C. It is equal to the centripetal force
  • D. It is equal to the sum of gravitational and centripetal forces
Q. If a satellite is launched into a higher orbit, how does its potential energy change compared to its initial orbit?
  • A. It decreases
  • B. It remains the same
  • C. It increases
  • D. It becomes zero
Q. If a satellite is moved to a higher orbit, what happens to its orbital period?
  • A. It decreases.
  • B. It increases.
  • C. It remains the same.
  • D. It becomes zero.
Q. If a satellite is moving in a circular orbit, what is the relationship between its centripetal acceleration and gravitational acceleration?
  • A. Centripetal = Gravitational
  • B. Centripetal > Gravitational
  • C. Centripetal < Gravitational
  • D. No relationship
Q. If a satellite is moving in a circular orbit, what type of energy does it possess?
  • A. Only kinetic energy
  • B. Only potential energy
  • C. Both kinetic and potential energy
  • D. Neither kinetic nor potential energy
Q. If a satellite's altitude is doubled, how does its orbital speed change?
  • A. Increases by √2
  • B. Decreases by √2
  • C. Remains the same
  • D. Increases by 2
Q. If a satellite's altitude is increased, what happens to its orbital period?
  • A. It decreases
  • B. It increases
  • C. It remains constant
  • D. It becomes zero
Q. If a satellite's speed is greater than the escape velocity, what will happen?
  • A. It will enter a stable orbit
  • B. It will escape Earth's gravitational pull
  • C. It will crash into the Earth
  • D. It will remain in a circular orbit
Q. If a satellite's speed is less than the required orbital speed, what will happen?
  • A. It will remain in orbit.
  • B. It will fall back to Earth.
  • C. It will escape into space.
  • D. It will move to a higher orbit.
Q. If the mass of a satellite is doubled while keeping its orbital radius constant, what happens to the gravitational force acting on it?
  • A. It doubles.
  • B. It remains the same.
  • C. It halves.
  • D. It quadruples.
Q. If the mass of the Earth is M and the radius is R, what is the gravitational force acting on a satellite of mass m at a height h?
  • A. GmM/R^2
  • B. GmM/(R+h)^2
  • C. GmM/(R-h)^2
  • D. GmM/h^2
Q. If the radius of the Earth is 6400 km, what is the total distance from the center of the Earth to a satellite in a geostationary orbit? (2000)
  • A. 36000 km
  • B. 42000 km
  • C. 32000 km
  • D. 28000 km
Q. If the radius of the Earth is R and a satellite is in a circular orbit at a height h above the Earth's surface, what is the expression for the orbital speed v of the satellite?
  • A. v = sqrt(GM/(R+h))
  • B. v = sqrt(GM/R)
  • C. v = sqrt(GM/(R-h))
  • D. v = sqrt(GM/(R^2 + h^2))
Q. If the radius of the Earth is R and a satellite is in a geostationary orbit, what is the height of the satellite above the Earth's surface?
  • A. R/2
  • B. R
  • C. R/3
  • D. R/4
Q. If the radius of the Earth is R and a satellite is in a low Earth orbit at a height h, what is the expression for the gravitational force acting on the satellite?
  • A. G * M * m / (R + h)^2
  • B. G * M * m / R^2
  • C. G * M * m / (R - h)^2
  • D. G * M * m / (R + h)
Q. If the radius of the Earth is R, what is the gravitational acceleration at a height R above the Earth's surface?
  • A. g/4
  • B. g/2
  • C. g
  • D. g/8
Q. If the radius of the Earth is R, what is the radius of a satellite in a geostationary orbit?
  • A. R
  • B. 2R
  • C. 3R
  • D. 4R
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Satellite Motion MCQ & Objective Questions

Understanding "Satellite Motion" is crucial for students preparing for various school and competitive exams. This topic not only forms a significant part of the physics syllabus but also helps in grasping fundamental concepts of motion and gravity. Practicing MCQs and objective questions on Satellite Motion can enhance your exam preparation, boost your confidence, and improve your chances of scoring better in exams.

What You Will Practise Here

  • Key concepts of satellite motion and its significance in physics.
  • Understanding the laws of planetary motion and gravitational force.
  • Formulas related to orbital velocity and period of satellites.
  • Types of satellites: geostationary and polar satellites.
  • Diagrams illustrating satellite orbits and trajectories.
  • Applications of satellites in communication and weather forecasting.
  • Common numerical problems related to satellite motion.

Exam Relevance

Satellite Motion is a recurring topic in CBSE, State Boards, NEET, and JEE exams. Students can expect questions that test their understanding of the laws governing satellite motion, calculations involving orbital speed, and the implications of satellite technology. Common question patterns include multiple-choice questions that require conceptual clarity and problem-solving skills, making it essential to practice thoroughly.

Common Mistakes Students Make

  • Confusing the concepts of geostationary and polar satellites.
  • Misapplying formulas related to orbital velocity and period.
  • Overlooking the significance of gravitational force in satellite motion.
  • Failing to interpret diagrams correctly, leading to errors in understanding orbits.

FAQs

Question: What is the difference between geostationary and polar satellites?
Answer: Geostationary satellites orbit the Earth at the same rotational speed, appearing stationary over one point, while polar satellites pass over the poles, providing global coverage.

Question: How do I calculate the orbital velocity of a satellite?
Answer: The orbital velocity can be calculated using the formula \( v = \sqrt{\frac{GM}{r}} \), where \( G \) is the gravitational constant, \( M \) is the mass of the Earth, and \( r \) is the distance from the center of the Earth to the satellite.

Now is the time to enhance your understanding of Satellite Motion! Dive into our practice MCQs and test your knowledge to excel in your exams. Remember, consistent practice is the key to success!

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