Physics, asked by pawannickkachhaph, 9 months ago

establish the following relations for a rocket v =Vo +Be In Mo/M​

Answers

Answered by panditshourya952445
0

Answer:

The thrust developed by a rocket-motor is given by F=mv+A(P

1

−P

2

) where m is the mass of the gas ejected per unit time, v is velocity of the gas, A is area of cross-section of the nozzle, P

1

and P

2

are the pressures of the exhaust gas and surrounding atmosphere. The formula is dimensionally

Similar questions