Vulnerability of Space Station Freedom Modules: A Study of the Effects of Module Perforation on Crew and Equipment
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0est aluminum ambient axial velocity bumper material calculated characteristic velocities DEB CLD INDUCED debris cloud components debris cloud impact debris cloud mass debris cloud material DEBRIS CLOUD PASSAGE density DIFF DEB CLD distance DOUBLE PRECISION drag coefficient equipment rack expansion velocity experimental results GM/CC GOTO Huntsville impact event IMPACT VELOCITY IMPEDANCE MATCH initial impact initial shock wave inner bumper INTERFACE internal debris cloud internal effects JOULES JOULES/KG kinetic energy KM/S leading edge velocity m/Sec MATL MELT Model Prediction module air momentum msec orbital debris overpressure particle velocity penetration perforation point of interest PRESS INCR pressure and temperature PRESSURE INCREASE pressure wall material primary debris cloud projectile and bumper RELEASE secondary debris cloud Section sensor position shield target SHOCK HEATING shock loading SHOCK VALUES shock wave induced SHOCK WAVE SPEED SHOCK WAVE VELOCITY spacecraft TEMP INCR TEMPERATURE INCREASE Test TOT TRANS WRITE X-COORD