{"title":"航天器惠普尔防护罩反应材料保险杠抗冲击机理的实验与数值模拟","authors":"Siyuan Ren , Qingming Zhang , Fang Gao , Qiang Wu , Haozhe Liang , Wenjin Liu , Xianzhe Zhong , Guangming Song","doi":"10.1016/j.ast.2022.107646","DOIUrl":null,"url":null,"abstract":"<div><p>With the rapid development of human manned spaceflight, the threat of hypervelocity impact of space debris to spacecraft safety has attracted more and more attention, and new materials for spacecraft shield need to be developed to meet the challenges caused by explosive growth of space debris. In this paper, the experiments of projectiles with hypervelocity impact on the Whipple shields with reactive material as bumpers were carried out by using two-stage light-gas gun. Through numerical simulations and experiments, the interaction between projectile and reactive material bumper was studied, and the fragments distribution, velocity and temperature of debris cloud induced by projectile impacting on reactive material bumper were analyzed. The hypervelocity impact resistance mechanism of Whipple shield with reactive material as bumper was obtained. The results show that the impact and detonation reaction combined effect of reactive material bumper can cause the projectile to be subjected to shock wave load twice, which leads to more effective fragmentation of projectile, more effective dispersion and deceleration of debris cloud, and more effective temperature rise of material. Reactive material bumper can improve the protective capability of Whipple shield, and has a great potential application prospect.</p></div>","PeriodicalId":50955,"journal":{"name":"Aerospace Science and Technology","volume":null,"pages":null},"PeriodicalIF":5.0000,"publicationDate":"2022-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":"{\"title\":\"Impact resistance mechanism of reactive material bumper for spacecraft Whipple shield: Experiments and numerical simulations\",\"authors\":\"Siyuan Ren , Qingming Zhang , Fang Gao , Qiang Wu , Haozhe Liang , Wenjin Liu , Xianzhe Zhong , Guangming Song\",\"doi\":\"10.1016/j.ast.2022.107646\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><p>With the rapid development of human manned spaceflight, the threat of hypervelocity impact of space debris to spacecraft safety has attracted more and more attention, and new materials for spacecraft shield need to be developed to meet the challenges caused by explosive growth of space debris. In this paper, the experiments of projectiles with hypervelocity impact on the Whipple shields with reactive material as bumpers were carried out by using two-stage light-gas gun. Through numerical simulations and experiments, the interaction between projectile and reactive material bumper was studied, and the fragments distribution, velocity and temperature of debris cloud induced by projectile impacting on reactive material bumper were analyzed. The hypervelocity impact resistance mechanism of Whipple shield with reactive material as bumper was obtained. The results show that the impact and detonation reaction combined effect of reactive material bumper can cause the projectile to be subjected to shock wave load twice, which leads to more effective fragmentation of projectile, more effective dispersion and deceleration of debris cloud, and more effective temperature rise of material. Reactive material bumper can improve the protective capability of Whipple shield, and has a great potential application prospect.</p></div>\",\"PeriodicalId\":50955,\"journal\":{\"name\":\"Aerospace Science and Technology\",\"volume\":null,\"pages\":null},\"PeriodicalIF\":5.0000,\"publicationDate\":\"2022-07-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"2\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Aerospace Science and Technology\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S1270963822003200\",\"RegionNum\":1,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q1\",\"JCRName\":\"ENGINEERING, AEROSPACE\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Aerospace Science and Technology","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S1270963822003200","RegionNum":1,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
Impact resistance mechanism of reactive material bumper for spacecraft Whipple shield: Experiments and numerical simulations
With the rapid development of human manned spaceflight, the threat of hypervelocity impact of space debris to spacecraft safety has attracted more and more attention, and new materials for spacecraft shield need to be developed to meet the challenges caused by explosive growth of space debris. In this paper, the experiments of projectiles with hypervelocity impact on the Whipple shields with reactive material as bumpers were carried out by using two-stage light-gas gun. Through numerical simulations and experiments, the interaction between projectile and reactive material bumper was studied, and the fragments distribution, velocity and temperature of debris cloud induced by projectile impacting on reactive material bumper were analyzed. The hypervelocity impact resistance mechanism of Whipple shield with reactive material as bumper was obtained. The results show that the impact and detonation reaction combined effect of reactive material bumper can cause the projectile to be subjected to shock wave load twice, which leads to more effective fragmentation of projectile, more effective dispersion and deceleration of debris cloud, and more effective temperature rise of material. Reactive material bumper can improve the protective capability of Whipple shield, and has a great potential application prospect.
期刊介绍:
Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to:
• The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites
• The control of their environment
• The study of various systems they are involved in, as supports or as targets.
Authors are invited to submit papers on new advances in the following topics to aerospace applications:
• Fluid dynamics
• Energetics and propulsion
• Materials and structures
• Flight mechanics
• Navigation, guidance and control
• Acoustics
• Optics
• Electromagnetism and radar
• Signal and image processing
• Information processing
• Data fusion
• Decision aid
• Human behaviour
• Robotics and intelligent systems
• Complex system engineering.
Etc.