Shield design, analysis, and testing to survive stainless steel projectiles
During the 3-year period of 1987 through 1989, the Advanced Shield Phenomenology Program included a research and development effort, with both experimental work and analytical support, to design a low weight, survivable shield against a stainless steel projectile at low earth orbit velocity. The specific threat used was a 1.75 gram, length to diameter ratio of one, stainless steel cylinder. The impact velocity was {approximately}7 km/s. Testing was performed at the Arnold Engineering Development Center, Arnold Air Force Base, Tullahoma, Tennessee. Sixteen shield configurations were tested. The Hull hydrocode was used for detailed analysis of five impact configurations. A successfulmore »