TY - JOUR
T1 - Velocity-space analysis method for hazardous fragments in debris clouds
AU - HE, Qi Guang
AU - Chen, Jin Fu
AU - Chen, Xiaowei
N1 - Publisher Copyright:
© 2021
PY - 2022/3
Y1 - 2022/3
N2 - A Whipple shield is a double-plate structure commonly used to protect space fragments from impacting spacecraft. The space fragment impacts the outer plate and is broken into a debris cloud with dispersed energy and momentum, which reduces the risk of penetrating the bulkhead. Hazardous fragments with greater mass and energy in the debris cloud are the main threats to the bulkhead. Based on the finite element and smoothed-particle hydrodynamics (FE-SPH) adaptive method, this study aims to establish a generic analysis method for hazardous fragments in the debris clouds, which includes identifying stable debris clouds, quantifying the lethality of hazardous fragments to the rear plate, determining the critical spacing of the double plate in the Whipple shield, describing the hazardous fragment distribution, and characterizing the energy angular distribution of hazardous fragments. The FE-SPH adaptive method enables the extraction of individual characteristics and distribution information of the hazardous fragments. The criteria of hazardous fragments are given based on the lethality of fragments on the rear plate. A quantitative criterion for a stable debris cloud (whose fragments are no longer breaking) was established, which provides a minimal double-plate spacing Lmin to ensure an effective Whipple structure. We introduce the velocity distribution of the fragments for analyzing the stable debris cloud. The maximum velocity angle θ99 of hazardous fragments is proposed to quantitatively analyze their distribution range. An orthogonal test shows that θ99 is related to the ratio of the plate thickness to the sphere diameter (H/D) and the projectile velocity V. Intensive test results indicate that θ99 is a function of V and H/D. By evaluating the applicable scope, the fitted function works well when the projectile is disintegrated. Finally, this study investigates the energy angular distribution of the hazardous fragments. The debris clouds are qualitatively divided into intact, ruptured, and disintegrated regions.
AB - A Whipple shield is a double-plate structure commonly used to protect space fragments from impacting spacecraft. The space fragment impacts the outer plate and is broken into a debris cloud with dispersed energy and momentum, which reduces the risk of penetrating the bulkhead. Hazardous fragments with greater mass and energy in the debris cloud are the main threats to the bulkhead. Based on the finite element and smoothed-particle hydrodynamics (FE-SPH) adaptive method, this study aims to establish a generic analysis method for hazardous fragments in the debris clouds, which includes identifying stable debris clouds, quantifying the lethality of hazardous fragments to the rear plate, determining the critical spacing of the double plate in the Whipple shield, describing the hazardous fragment distribution, and characterizing the energy angular distribution of hazardous fragments. The FE-SPH adaptive method enables the extraction of individual characteristics and distribution information of the hazardous fragments. The criteria of hazardous fragments are given based on the lethality of fragments on the rear plate. A quantitative criterion for a stable debris cloud (whose fragments are no longer breaking) was established, which provides a minimal double-plate spacing Lmin to ensure an effective Whipple structure. We introduce the velocity distribution of the fragments for analyzing the stable debris cloud. The maximum velocity angle θ99 of hazardous fragments is proposed to quantitatively analyze their distribution range. An orthogonal test shows that θ99 is related to the ratio of the plate thickness to the sphere diameter (H/D) and the projectile velocity V. Intensive test results indicate that θ99 is a function of V and H/D. By evaluating the applicable scope, the fitted function works well when the projectile is disintegrated. Finally, this study investigates the energy angular distribution of the hazardous fragments. The debris clouds are qualitatively divided into intact, ruptured, and disintegrated regions.
KW - Debris cloud
KW - Distribution of hazardous fragments
KW - Energy angular distribution
KW - FE–SPH adaptive method
KW - Maximum velocity angle
KW - Velocity space
UR - http://www.scopus.com/inward/record.url?scp=85120338361&partnerID=8YFLogxK
U2 - 10.1016/j.ijimpeng.2021.104087
DO - 10.1016/j.ijimpeng.2021.104087
M3 - Article
AN - SCOPUS:85120338361
SN - 0734-743X
VL - 161
JO - International Journal of Impact Engineering
JF - International Journal of Impact Engineering
M1 - 104087
ER -