Derive the velocity equation of rocket propulsion
Answers
Answered by
1
Answer:
hey mate here your answer:
- the propulsion of rocket is the law of conservative of linear momentum of Newton's third law
- the rocket are filled with either solid or liquid
- when the rocket is fly the hot gas ejected from the high speed nozzle in the prop a lent tank
hope it help you
Answered by
0
Δ v = u ln ( m i m ) . This result is called the rocket equation. It was originally derived by the Soviet physicist Konstantin Tsiolkovsky in 1897. It gives us the change of velocity that the rocket obtains from burning a mass of fuel that decreases the total rocket mass from m0 down to m...
✔❤️❤️
Similar questions
Social Sciences,
5 months ago
Math,
5 months ago
Political Science,
10 months ago
Chemistry,
1 year ago
Math,
1 year ago