A Collection of Technical Papers: AIAA Fifth Annual Structures and Materials Conference, Palm Springs, California, Riviera Hotel, April 1-3, 1964 |
Contents
PAGE | 7 |
HYPERVELOCITY IMPACT STUDIES CONCERNING THE METEOROID | 78 |
R A Needham and M A Steinberg Lockheed Missiles and Space | 105 |
13 other sections not shown
Common terms and phrases
ablator aerodynamic alloys aluminum analysis applied approximately axial basic bending booster boundary coefficient components compression configuration constant crack creep strain curves cylinder deformation density determined diameter dynamic effect elastic elastomer equation evaluation experimental factor of safety fiber metal filaments filler FINENESS RATIO flight flutter foam frequency function honeycomb Hypervelocity impact inch increase insulation launch lift linear load cycles longitudinal Mach number mass fraction material Mercury-Atlas meteoroid method mode mode shapes modulus NASA Nondimensional normal obtained panels parameter payload penetration plastic pressure problem projectile propellant pyrolytic graphite range ratio re-entry residual stresses Reynolds number sandwich shear sheet shell shown in Figure simulation skin solution space steady stress stiffness stress concentrations structural weight subliming surface tank target theory thermal conductivity thermal stresses thickness tion titanium unsteady values variables vehicle velocity vibration zero