Rm. Schmidt et al., CADMIUM SIMULATION OF ORBITAL-DEBRIS SHIELD PERFORMANCE TO SCALED VELOCITIES OF 18-KM S/, Journal of spacecraft and rockets, 31(5), 1994, pp. 866-877
An experimental technique is developed and used to simulate the respon
se of aluminum debris shields for impacts up to 18 km/s. To simulate a
n aluminum impact on an aluminum shield, the velocity is reduced by a
scale factor, and the impactor and bumper are surrogates that have the
same dimensions as the originals, but are composed of a material whos
e specific energies of melting and vaporization are much lower than th
ose of aluminum. Cadmium is used as the surrogate material, because it
has unique properties that satisfy the attendant scaling requirements
and because its velocity scale factor is 3.1, thereby allowing tests
at actual velocities up to 5.8 km/s to simulate aluminum impacts at ve
locities up to 18 km/s. Such tests reproduce the initial momentum of a
n aluminum impactor and the impulse distribution delivered to the rear
wall. Cadmium tests, at scaled velocities near 7 km/s, agreed well wi
th aluminum tests near 7 km/s, both in terms of debris cloud geometry
and the minimum impactor size for wall perforation. Simulations at hig
her scaled velocities showed that the minimum diameter for penetration
increases with increasing velocities above 10.5 km/s, in sharp contra
st to current empirical shield models.