Enhanced hypervelocity launcher - Capabilities to 16 km/s

被引:84
作者
Chhabildas, LC
Kmetyk, LN
Reinhart, WD
Hall, CA
机构
[1] Sandia National Laboratories Experimental Impact Physics Department Albuquerque
关键词
D O I
10.1016/0734-743X(95)99845-I
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
A systematic study is described which has led to the successful launch of thin flier plates to velocities of 16 km/s. The energy required to launch a flier plate to 16 km/s is approximately 10 to 15 times the energy required to melt and vaporize the plate. The energy must, therefore, be deposited in a well-controlled manner to prevent melt or vaporization. This is achieved by using a graded-density assembly to impact a stationary flier-plate. Upon impact, time-dependent, structured, high pressure pulses are generated and used to propel the plates to hypervelocities without melt or fracture. In previous studies, a graded-density impact of 7.3 km/s was used to launch a 0.5 mm thick plate to a velocity of over 12 km/s. If impact techniques alone were to be used to achieve flier-plate velocities approaching 16 km/s, this would require that the graded-density impact occur at similar to 10 km/s. In this paper, we describe a new technique that has been implemented to enhance the performance of the Sandia hypervelocity launcher. This technique of creating an impact-generated acceleration reservoir, has allowed the launch of 0.5 mm to 1.0 mm thick plates to record velocities up to 15.8 km/s. In these experiments, both titanium (Ti-6Al-4V) and aluminum (6061-T6) alloy were used for the flier-plate material. These are the highest metallic projectile plate velocities ever achieved for masses in the range of 0.1 g to 1 g.
引用
收藏
页码:183 / 194
页数:12
相关论文
共 22 条
[1]  
ANG JA, 1992, AIAA92159014 PAP
[2]   THE USE OF HYPERVELOCITY LAUNCHERS TO EXPLORE PREVIOUSLY INACCESSIBLE STATES OF MATTER [J].
ASAY, JR ;
TRUCANO, TG ;
HAWKE, RS .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 1990, 10 (1-4) :51-66
[3]  
ASAY JR, 1985, SAND852009 SAND NAT
[4]   LASER INTERFEROMETER FOR MEASURING HIGH VELOCITIES OF ANY REFLECTING SURFACE [J].
BARKER, LM ;
HOLLENBACH, RE .
JOURNAL OF APPLIED PHYSICS, 1972, 43 (11) :4669-+
[5]   HYPERVELOCITY TESTING OF ADVANCED SHIELDING CONCEPTS FOR SPACECRAFT AGAINST IMPACTS TO 10-KM/S [J].
BOSLOUGH, MB ;
ANG, JA ;
CHHABILDAS, LC ;
REINHART, WD ;
HALL, CA ;
COURPALAIS, BG ;
CHRISTIANSEN, EL ;
CREWS, JL .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 1993, 14 (1-4) :95-106
[6]  
BRANNON RM, 1994, INT J IMPACT ENG, P109
[7]  
BUCHANAN TL, 1993, AEDCTR9314
[8]  
Charters A.C., 1987, INT J IMPACT ENG, V5, P181, DOI [DOI 10.1016/0734-743X(87)90038-8, 10.1016/0734-743x(87)90038-8]
[9]  
Chhabildas L. C., 1990, Shock Compression of Condensed Matter - 1989. Proceedings of the American Physical Society Topical Conference, P429
[10]  
Chhabildas L. C., 1992, RECENT TRENDS HIGH P, P739