Accession Number : AD0421685

Title :   LEADING EDGES DEVELOPMENT - DYNA SOAR. VOLUME 3 THERMAL GRADIENT AND LOADS TEST DATA

Corporate Author : BOEING CO SEATTLE WA

Personal Author(s) : Bowers, D A ; Esch, Paul G

PDF Url : AD0421685

Report Date : 25 Jun 1963

Pagination or Media Count : 325

Abstract : Contents: tabulated temperature data, tabulated pressure load vs. deflection data, tabulated pressure load vs. maximum shear stress and principal stress data, rapid load vs. time curves, tabulated rapid load vs. deflection data, tabulated slow load vs. deflection data, and tolerances for thermocouples.

Descriptors :   *BOOST GLIDE VEHICLES, AERODYNAMIC HEATING, AERODYNAMIC LOADING, DEFLECTION, DELTA WINGS, EXPERIMENTAL DATA, LEADING EDGE FLAPS, LOAD DISTRIBUTION, MANNED SPACECRAFT, PRESSURE, SHEAR STRESSES, TABLES(DATA), TEMPERATURE, THERMOCOUPLES, TIME

Subject Categories : Unmanned Spacecraft

Distribution Statement : APPROVED FOR PUBLIC RELEASE