smallcattle
Member
early astronauts in space only orbited the Earth at an altitude of between 80km and 200km. A typical rocket engine would provide a thrust of 380000N to a rocket with a total mass of 29830kg prior to lift off and would use 25315kg of fuel during the flight
Q: assuming the thrust is kept constant, calculate the final acceleration of this rocket immediately before the fuel would had been used
how to calculate the final acceleration???
Q: assuming the thrust is kept constant, calculate the final acceleration of this rocket immediately before the fuel would had been used
how to calculate the final acceleration???