Launch Performance Degradation of the Rupture-Type Missile Canister
This paper describes the degradation of launch performance caused by the remnants of a missile canister cover with a sabot interface, on interference with adjacent structures. First, by including the material plastic behavior and element deletion, we predict interference between the structures and t...
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doaj-8d520434aa364ababe67feab13b9bdf42020-11-24T20:54:53ZengMDPI AGApplied Sciences2076-34172019-03-0197129010.3390/app9071290app9071290Launch Performance Degradation of the Rupture-Type Missile CanisterWonhong Choi0Sunghun Jung1Department of Mechanical Engineering, Purdue University, West Lafayette, IN 47907, USADepartment of Electric Vehicle Engineering, Dongshin University, Najusi, Jeonnam 58245, KoreaThis paper describes the degradation of launch performance caused by the remnants of a missile canister cover with a sabot interface, on interference with adjacent structures. First, by including the material plastic behavior and element deletion, we predict interference between the structures and the detached part, followed by excessive deformation. Second, we verify that the support ring deformation, which is induced by an interaction with the cover remains, increases for fastener separations with abnormal fastener installations. This increase further triggers interference with the boosters on the bottom of a missile. Lastly, we analyze the variation of material property in a high-speed environment.https://www.mdpi.com/2076-3417/9/7/1290finite element analysis (FEA)impact behaviormissile canister |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Wonhong Choi Sunghun Jung |
spellingShingle |
Wonhong Choi Sunghun Jung Launch Performance Degradation of the Rupture-Type Missile Canister Applied Sciences finite element analysis (FEA) impact behavior missile canister |
author_facet |
Wonhong Choi Sunghun Jung |
author_sort |
Wonhong Choi |
title |
Launch Performance Degradation of the Rupture-Type Missile Canister |
title_short |
Launch Performance Degradation of the Rupture-Type Missile Canister |
title_full |
Launch Performance Degradation of the Rupture-Type Missile Canister |
title_fullStr |
Launch Performance Degradation of the Rupture-Type Missile Canister |
title_full_unstemmed |
Launch Performance Degradation of the Rupture-Type Missile Canister |
title_sort |
launch performance degradation of the rupture-type missile canister |
publisher |
MDPI AG |
series |
Applied Sciences |
issn |
2076-3417 |
publishDate |
2019-03-01 |
description |
This paper describes the degradation of launch performance caused by the remnants of a missile canister cover with a sabot interface, on interference with adjacent structures. First, by including the material plastic behavior and element deletion, we predict interference between the structures and the detached part, followed by excessive deformation. Second, we verify that the support ring deformation, which is induced by an interaction with the cover remains, increases for fastener separations with abnormal fastener installations. This increase further triggers interference with the boosters on the bottom of a missile. Lastly, we analyze the variation of material property in a high-speed environment. |
topic |
finite element analysis (FEA) impact behavior missile canister |
url |
https://www.mdpi.com/2076-3417/9/7/1290 |
work_keys_str_mv |
AT wonhongchoi launchperformancedegradationoftherupturetypemissilecanister AT sunghunjung launchperformancedegradationoftherupturetypemissilecanister |
_version_ |
1716793412272783360 |