Hypervelocity Impact Testing of a Metallic Glass-Stuffed Whipple Shield

2015 ◽  
Vol 17 (9) ◽  
pp. 1313-1322 ◽  
Author(s):  
Douglas C. Hofmann ◽  
Lee Hamill ◽  
Eric Christiansen ◽  
Steve Nutt
2010 ◽  
Vol 452-453 ◽  
pp. 385-388
Author(s):  
Bin Jia ◽  
Gao Jian Liao ◽  
Hai Peng Gong ◽  
Bao Jun Pang

All spacecrafts in earth orbit are subject to hypervelocity impact by micro-meteoroids and space debris, which can in turn lead to significant damage and catastrophic failure of spacecraft. Porous volcano rock was adopted as one of micro-meteoroid material due to their similar physical and geometric features. Two-stage light gas gun experiments were carried out for a 6mm diameter volcano rock projectile impact on an Al-Whipple shield within the speed range from 1 km/s to 3 km/s. An ANSYS/LS-DYNA software was employed and justified by experimental results, in which a porous geometrical model was established for volcano rock projectile. The higher speed range was extended from 3 km/s to 10 km/s by numerical simulation. The results of experiments and numerical simulation indicated that major damage on rear wall of the Whipple shield impacted by volcano rock projectile is caused by the fragments of bumper of the shield, which is different from that of aluminum projectile. And 5.5km/s is the critical speed of a 6mm diameter volcano rock projectile impact on the Whipple shield investigated.


2019 ◽  
Vol 304 ◽  
pp. 07003
Author(s):  
Martin Schubert ◽  
Anthanasios Dafnis

In the project multiSat multifunctional composite structures for satellite application have been developed. Functions such as protection against space debris, radiation shielding and passive thermal control have been integrated into the load-bearing composite spacecraft structure by use of suitable materials and components. Sandwich panels have been studied as representative structural parts of a conventional satellite structure. Measures for increased space debris protection include the substitution of the conventional honeycomb core by 3D-printed aluminum cellular structures and the reinforcement of the sandwich panel by integration of high performance fabrics which effectively break up and catch impacting debris particles. This paper describes the development and design of multifunctional sandwich concepts with increased impact protection capability and presents the experimental results of hypervelocity impact testing with different types of CFRP sandwich panels.


1996 ◽  
Author(s):  
Eric L. Christiansen ◽  
Jeanne Lee Crews ◽  
Justin H. Kerr ◽  
Lalit C. Chhabildas

2016 ◽  
Vol 119 ◽  
pp. 48-59 ◽  
Author(s):  
Xiaotian Zhang ◽  
Tao Liu ◽  
Xiaogang Li ◽  
Guanghui Jia

2017 ◽  
Vol 204 ◽  
pp. 390-396 ◽  
Author(s):  
Erick Ordonez ◽  
Jennifer Edmunson ◽  
Michael Fiske ◽  
Eric Christiansen ◽  
Joshua Miller ◽  
...  

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