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

被引:19
作者
SCHMIDT, RM [1 ]
HOUSEN, KR [1 ]
PIEKUTOWSKI, AJ [1 ]
POORMAN, KL [1 ]
机构
[1] UNIV DAYTON,RES INST,DAYTON,OH 45469
关键词
D O I
10.2514/3.26525
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
An experimental technique is developed and used to simulate the response of aluminum debris shields for impacts up to 18 km/s. To simulate an 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 whose specific energies of melting and vaporization are much lower than those 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 velocities up to 18 km/s. Such tests reproduce the initial momentum of an aluminum impactor and the impulse distribution delivered to the rear wall. Cadmium tests, at scaled velocities near 7 km/s, agreed well with aluminum tests near 7 km/s, both in terms of debris cloud geometry and the minimum impactor size for wall perforation. Simulations at higher scaled velocities showed that the minimum diameter for penetration increases with increasing velocities above 10.5 km/s, in sharp contrast to current empirical shield models.
引用
收藏
页码:866 / 877
页数:12
相关论文
共 23 条
[1]  
ANG JA, 1992, AIAA921590 PAP
[2]  
CHHABILDAS LC, 1992, AIAA921639 PAP
[3]   DESIGN AND PERFORMANCE EQUATIONS FOR ADVANCED METEOROID AND DEBRIS SHIELDS [J].
CHRISTIANSEN, EL .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 1993, 14 (1-4) :145-156
[4]  
CHRISTIANSEN EL, 1990, JSC SN39119 JOHNS SP
[5]  
GEHRING JW, 1970, HIGH VELOCITY IMPACT, P105
[6]  
HILL SA, 1991, COMP WHIPPLE SHIELD
[7]   HYPERVELOCITY IMPACT EXPERIMENTS IN SURROGATE MATERIALS [J].
HOLSAPPLE, KA .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 1993, 14 (1-4) :335-345
[8]   MATERIAL PHASE-TRANSFORMATION EFFECTS UPON PERFORMANCE OF SPACED BUMPER SYSTEMS [J].
HOPKINS, AK ;
SWIFT, HF ;
LEE, TW .
JOURNAL OF SPACECRAFT AND ROCKETS, 1972, 9 (05) :342-&
[9]  
KESSLER DJ, 1988, NASA TM100471
[10]  
LAWRENCE RJ, 1992, AIAA921465 PAP