DYNAMIC PRESSURE DECAY AFTER THRUST TERMINATION.
Technical operating rept.,
AEROSPACE CORP EL SEGUNDO CA EL SEGUNDO TECHNICAL OPERATIONS
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The dynamic pressure time history after thrust termination is shown to be represented by a simple analytical approximation derived from powered flight trajectory parameters. The approximation is correlated with the results of accurate trajectory simulations. The agreement is adequate for ride-out abort escape studies. Author
- Rocket Engines