For a rocket propulsion velocity of exhaust gases relative to rocket is 2km/s.If mass of rocket system is 1000kg,then what is the rate of fuel consumption for a rocket to rise up with acceleration 4.9m/s^2?
Finding a professional expert in "partial differential equations" in the advanced level is difficult.
You can find this expert in "Assignmentexpert.com" with confidence.
Exceptional experts! I appreciate your help. God bless you!
Comments
Dear Arnav, net acceleration of the rocket is 4.9m/s^2
Why is net acceleration= a+g