Accession Number:

AD0805371

Title:

DYNAMIC PRESSURE DECAY AFTER THRUST TERMINATION.

Descriptive Note:

Technical operating rept.,

Corporate Author:

AEROSPACE CORP EL SEGUNDO CA EL SEGUNDO TECHNICAL OPERATIONS

Personal Author(s):

Report Date:

1965-08-02

Pagination or Media Count:

11.0

Abstract:

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

Subject Categories:

  • Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE