Safety Assessment of a Metal Cask under Aircraft Engine Crash

The structural integrity of a dual-purpose metal cask currently under development by the Korea Radioactive Waste Agency (KORAD) was evaluated, through numerical simulations and a model test, under high-speed missile impact reflecting targeted aircraft crash conditions. The impact conditions were car...

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Main Authors: Sanghoon Lee, Woo-Seok Choi, Ki-Seog Seo
Format: Article
Language:English
Published: Elsevier 2016-04-01
Series:Nuclear Engineering and Technology
Subjects:
Online Access:http://www.sciencedirect.com/science/article/pii/S1738573315002272
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spelling doaj-10c6d44a3cd24bc7ad4e40dd3261f82c2020-11-24T23:19:31ZengElsevierNuclear Engineering and Technology1738-57332016-04-0148250551710.1016/j.net.2015.11.002Safety Assessment of a Metal Cask under Aircraft Engine CrashSanghoon Lee0Woo-Seok Choi1Ki-Seog Seo2Department of Mechanical and Automotive Engineering, Keimyung University, Dalgubeol-daero 1095, Dalseo-gu, Daegu 42601, Republic of KoreaKorea Atomic Energy Research Institute, Daedeok-daero 989-111, Yuseong-gu, Daejeon 34057, Republic of KoreaKorea Atomic Energy Research Institute, Daedeok-daero 989-111, Yuseong-gu, Daejeon 34057, Republic of KoreaThe structural integrity of a dual-purpose metal cask currently under development by the Korea Radioactive Waste Agency (KORAD) was evaluated, through numerical simulations and a model test, under high-speed missile impact reflecting targeted aircraft crash conditions. The impact conditions were carefully chosen through a survey on accident cases and recommendations from literature. In the impact scenario, a missile flying horizontally hits the top side of the cask, which is freestanding on a concrete pad, with a velocity of 150 m/s. A simplified missile simulating a commercial aircraft engine was designed from an impact load–time function available in literature. In the analyses, the dynamic behavior of the metal cask and the integrity of the containment boundary were assessed. The simulation results were compared with the test results for a 1:3 scale model. Although the dynamic behavior of the cask in the model test did not match exactly with the prediction from the numerical simulation, other structural responses, such as the acceleration and strain history during the impact, showed very good agreement. Moreover, the containment function of the cask survived the missile impact as expected from the numerical simulation. Thus, the procedure and methodology adopted in the structural numerical analyses were successfully validated.http://www.sciencedirect.com/science/article/pii/S1738573315002272High-Speed ImpactSafetySpent Nuclear FuelStorage CaskTargeted Aircraft Crash
collection DOAJ
language English
format Article
sources DOAJ
author Sanghoon Lee
Woo-Seok Choi
Ki-Seog Seo
spellingShingle Sanghoon Lee
Woo-Seok Choi
Ki-Seog Seo
Safety Assessment of a Metal Cask under Aircraft Engine Crash
Nuclear Engineering and Technology
High-Speed Impact
Safety
Spent Nuclear Fuel
Storage Cask
Targeted Aircraft Crash
author_facet Sanghoon Lee
Woo-Seok Choi
Ki-Seog Seo
author_sort Sanghoon Lee
title Safety Assessment of a Metal Cask under Aircraft Engine Crash
title_short Safety Assessment of a Metal Cask under Aircraft Engine Crash
title_full Safety Assessment of a Metal Cask under Aircraft Engine Crash
title_fullStr Safety Assessment of a Metal Cask under Aircraft Engine Crash
title_full_unstemmed Safety Assessment of a Metal Cask under Aircraft Engine Crash
title_sort safety assessment of a metal cask under aircraft engine crash
publisher Elsevier
series Nuclear Engineering and Technology
issn 1738-5733
publishDate 2016-04-01
description The structural integrity of a dual-purpose metal cask currently under development by the Korea Radioactive Waste Agency (KORAD) was evaluated, through numerical simulations and a model test, under high-speed missile impact reflecting targeted aircraft crash conditions. The impact conditions were carefully chosen through a survey on accident cases and recommendations from literature. In the impact scenario, a missile flying horizontally hits the top side of the cask, which is freestanding on a concrete pad, with a velocity of 150 m/s. A simplified missile simulating a commercial aircraft engine was designed from an impact load–time function available in literature. In the analyses, the dynamic behavior of the metal cask and the integrity of the containment boundary were assessed. The simulation results were compared with the test results for a 1:3 scale model. Although the dynamic behavior of the cask in the model test did not match exactly with the prediction from the numerical simulation, other structural responses, such as the acceleration and strain history during the impact, showed very good agreement. Moreover, the containment function of the cask survived the missile impact as expected from the numerical simulation. Thus, the procedure and methodology adopted in the structural numerical analyses were successfully validated.
topic High-Speed Impact
Safety
Spent Nuclear Fuel
Storage Cask
Targeted Aircraft Crash
url http://www.sciencedirect.com/science/article/pii/S1738573315002272
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AT wooseokchoi safetyassessmentofametalcaskunderaircraftenginecrash
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