Let (Vo) and (Ve) represent the orbital velocity and escape velocity of a satellite corresponding to a circular orbit of radius R. Derive the relation between them
Share
Let (Vo) and (Ve) represent the orbital velocity and escape velocity of a satellite corresponding to a circular orbit of radius R. Derive the relation between them
Sign Up to our social questions and Answers Engine to ask questions, answer people’s questions, and connect with other people.
Login to our social questions & Answers Engine to ask questions answer people’s questions & connect with other people.
Using the Conservation of Energy, we can derive the Escape Velocity as:
Now, For Orbital Velocity
Dividing Both The Equations:
If R=Radius of Earth
Answer:
hii
Explanation:
have a great day ahead ✌️✌️✌️ Rohan