Delta_Glider
New member
- Joined
- Jun 6, 2010
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Hi Orbinauts,
I am doing some practice flight planning from first-principles, i.e. using my own calculations with a python script and not punching numbers into MFDs.
Looking at the ideal rocket equation, I'd like to know the specific impulse of the main engines of the DG and Shuttle-A, and how they vary with atmospheric pressure. I cannot seem to find this information in the reference documents. Can anybody point me in the right direction ?
Cheers!
I am doing some practice flight planning from first-principles, i.e. using my own calculations with a python script and not punching numbers into MFDs.
Looking at the ideal rocket equation, I'd like to know the specific impulse of the main engines of the DG and Shuttle-A, and how they vary with atmospheric pressure. I cannot seem to find this information in the reference documents. Can anybody point me in the right direction ?
Cheers!