I want to be able to model the entire launch mission of the spacecraft GOES-O and its Launcher, Delta 4,2 medium plus.
Is it in anyway possible to obtain:-
- The burn profile, (simplified ones are fine like constant burn rate, constant acceleration, etc.).
- The time at which the gravity turn starts, along with the information about how does the rate of change of angle from vertical take place.
- The final velocity, position and angle where the spacecraft is released, for eg. GOES-O, in my case. So that I can calculate the further maneuvers on my own.
I have tried searching on the official NASA site, but couldn't get a clear information.
I need to obtain the parameters so that I can broadly comment upon the Trajectory followed by the rocket.
It would be great if someone could provide me with the links or any such related information from their knowledge. I require it for my Project.