A 3500-kg rocket is to be accelerated at 3.0 g at
Chapter 9, Problem 9.80(choose chapter or problem)
A 3500-kg rocket is to be accelerated at 3.0 g at take-offfrom the Earth. If the gases can be ejected at a rate of27 kg/s, what must be their exhaust speed?
Unfortunately, we don't have that question answered yet. But you can get it answered in just 5 hours by Logging in or Becoming a subscriber.
Becoming a subscriber
Or look for another answer