CADMIUM SIMULATION OF ORBITAL-DEBRIS SHIELD PERFORMANCE TO SCALED VELOCITIES OF 18-KM S/

Citation
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
Citations number
23
Categorie Soggetti
Aerospace Engineering & Tecnology
ISSN journal
00224650
Volume
31
Issue
5
Year of publication
1994
Pages
866 - 877
Database
ISI
SICI code
0022-4650(1994)31:5<866:CSOOSP>2.0.ZU;2-3
Abstract
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.