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Trying to make a simplified potential range estimate. The thing is that due to the scramjet propulsion, treating it similar as rocket would be false. My approach however is to use rocket equation to predict the boost speed, range and burnout altitude then followed by Breguet range equation to predict potential range in the horizontal flight.I wonder if such approach sufficient for at least early estimate.
Trying to make a simplified potential range estimate. The thing is that due to the scramjet propulsion, treating it similar as rocket would be false. My approach however is to use rocket equation to predict the boost speed, range and burnout altitude then followed by Breguet range equation to predict potential range in the horizontal flight.
I wonder if such approach sufficient for at least early estimate.
