Orbiter Thermal Pressure Drop Characteristics for Shuttle Orbiter Thermal Protection System Components:High Density Tile,Low Density Tile, Densified Low Density Tile,and Strain Isolation Pad.

摘要

Pressure drop tests were conducted on available samples of low and high density tile, densified low density tile, and strain isolation pads. The results are presented in terms of pressure drop, material thickness and volume flow rate. Although the test apparatus was only capable of a small part of the range of conditions to be encountered in a Shuttle Orbiter flight, the data serve to determine the type of flow characteristics to be expected for each material type tested; the measured quantities also should serve as input for initial venting and flow through analysis.