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A launching vehicle carrying an artificial’ satellite of mass m is set for launch on the surface of the earth of mass M and radius R. If the satellite is intended to move in a circular orbit of radius 7 R, the minimum energy required to be spent by the launching vehicle onthe satellite is (Gravitational constant = G)
- a)GMm / R
- b)– 13 GMm/14R
- c)GMm/7 R
- d)– GMm / 14R
Correct answer is option 'B'. Can you explain this answer?
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Satellite is a complex system that involves multiple stages, engines, and components. The primary function of the launching vehicle is to provide enough thrust and velocity to overcome Earth's gravity and launch the satellite into orbit.
The launching vehicle typically consists of three main stages: the first stage, second stage, and third stage. The first stage is usually the largest and most powerful, and it provides the initial thrust to lift the vehicle off the ground. Once the first stage has burned out and separated, the second stage takes over and continues to accelerate the vehicle to a higher altitude and speed. Finally, the third stage is responsible for placing the satellite into its final orbit.
Each stage is powered by one or more rocket engines, which burn a combination of fuel and oxidizer to create a high-pressure exhaust stream that propels the vehicle forward. The specific type of engine and fuel used can vary depending on the mission requirements and the design of the launching vehicle.
In addition to the stages and engines, the launching vehicle also has various other components such as guidance systems, avionics, and structural support systems. These components are critical to ensuring the vehicle stays on course and withstands the intense forces of launch and flight.
Overall, launching a satellite into orbit is a complex and challenging process that requires careful planning, engineering, and execution. However, the benefits of space-based technology and exploration make it a worthwhile endeavor for many governments, companies, and organizations.
The launching vehicle typically consists of three main stages: the first stage, second stage, and third stage. The first stage is usually the largest and most powerful, and it provides the initial thrust to lift the vehicle off the ground. Once the first stage has burned out and separated, the second stage takes over and continues to accelerate the vehicle to a higher altitude and speed. Finally, the third stage is responsible for placing the satellite into its final orbit.
Each stage is powered by one or more rocket engines, which burn a combination of fuel and oxidizer to create a high-pressure exhaust stream that propels the vehicle forward. The specific type of engine and fuel used can vary depending on the mission requirements and the design of the launching vehicle.
In addition to the stages and engines, the launching vehicle also has various other components such as guidance systems, avionics, and structural support systems. These components are critical to ensuring the vehicle stays on course and withstands the intense forces of launch and flight.
Overall, launching a satellite into orbit is a complex and challenging process that requires careful planning, engineering, and execution. However, the benefits of space-based technology and exploration make it a worthwhile endeavor for many governments, companies, and organizations.
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A launching vehicle carrying an artificial’ satellite of mass m is set for launch on the surface of the earth of mass M and radius R. If the satellite is intended to move in a circular orbit of radius 7 R, the minimum energy required to be spent by the launching vehicle onthe satellite is (Gravitational constant = G)a)GMm / Rb)– 13 GMm/14Rc)GMm/7 Rd)– GMm / 14RCorrect answer is option 'B'. Can you explain this answer?
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A launching vehicle carrying an artificial’ satellite of mass m is set for launch on the surface of the earth of mass M and radius R. If the satellite is intended to move in a circular orbit of radius 7 R, the minimum energy required to be spent by the launching vehicle onthe satellite is (Gravitational constant = G)a)GMm / Rb)– 13 GMm/14Rc)GMm/7 Rd)– GMm / 14RCorrect answer is option 'B'. Can you explain this answer? for NEET 2024 is part of NEET preparation. The Question and answers have been prepared according to the NEET exam syllabus. Information about A launching vehicle carrying an artificial’ satellite of mass m is set for launch on the surface of the earth of mass M and radius R. If the satellite is intended to move in a circular orbit of radius 7 R, the minimum energy required to be spent by the launching vehicle onthe satellite is (Gravitational constant = G)a)GMm / Rb)– 13 GMm/14Rc)GMm/7 Rd)– GMm / 14RCorrect answer is option 'B'. Can you explain this answer? covers all topics & solutions for NEET 2024 Exam. Find important definitions, questions, meanings, examples, exercises and tests below for A launching vehicle carrying an artificial’ satellite of mass m is set for launch on the surface of the earth of mass M and radius R. If the satellite is intended to move in a circular orbit of radius 7 R, the minimum energy required to be spent by the launching vehicle onthe satellite is (Gravitational constant = G)a)GMm / Rb)– 13 GMm/14Rc)GMm/7 Rd)– GMm / 14RCorrect answer is option 'B'. Can you explain this answer?.
A launching vehicle carrying an artificial’ satellite of mass m is set for launch on the surface of the earth of mass M and radius R. If the satellite is intended to move in a circular orbit of radius 7 R, the minimum energy required to be spent by the launching vehicle onthe satellite is (Gravitational constant = G)a)GMm / Rb)– 13 GMm/14Rc)GMm/7 Rd)– GMm / 14RCorrect answer is option 'B'. Can you explain this answer? for NEET 2024 is part of NEET preparation. The Question and answers have been prepared according to the NEET exam syllabus. Information about A launching vehicle carrying an artificial’ satellite of mass m is set for launch on the surface of the earth of mass M and radius R. If the satellite is intended to move in a circular orbit of radius 7 R, the minimum energy required to be spent by the launching vehicle onthe satellite is (Gravitational constant = G)a)GMm / Rb)– 13 GMm/14Rc)GMm/7 Rd)– GMm / 14RCorrect answer is option 'B'. Can you explain this answer? covers all topics & solutions for NEET 2024 Exam. Find important definitions, questions, meanings, examples, exercises and tests below for A launching vehicle carrying an artificial’ satellite of mass m is set for launch on the surface of the earth of mass M and radius R. If the satellite is intended to move in a circular orbit of radius 7 R, the minimum energy required to be spent by the launching vehicle onthe satellite is (Gravitational constant = G)a)GMm / Rb)– 13 GMm/14Rc)GMm/7 Rd)– GMm / 14RCorrect answer is option 'B'. Can you explain this answer?.
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