Accession Number:

AD0718560

Title:

Aerodynamic Heating

Descriptive Note:

Materiel test procedure rept.

Corporate Author:

ARMY TEST AND EVALUATION COMMAND ABERDEEN PROVING GROUND MD

Personal Author(s):

Report Date:

1967-07-24

Pagination or Media Count:

32.0

Abstract:

The objective of this MTP is to determine the effect of high temperature and temperature changes, resulting from aerodynamic heating, on the missile skin, structure, and interior components using laboratory methods. Such information is used to determine the adequacy of equipment to meet specified requirements such as the ability to withstand the aerodynamic heating associated with flying a specified trajectory. Author

Subject Categories:

  • Test Facilities, Equipment and Methods
  • Guided Missiles
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE