Journal of Space Safety Engineering最新文献_第8页

Legal challenges to the operation and use of commercial spaceports 商业航天港运营和使用面临的法律挑战

Journal of Space Safety Engineering Pub Date : 2024-06-01 DOI: 10.1016/j.jsse.2024.02.005

Yuri Takaya

引用次数: 0

IAASS supports international commitments to not conduct destructive anti-satellite testing 国际空间安全促进协会支持不进行破坏性反卫星试验的国际承诺

Journal of Space Safety Engineering Pub Date : 2024-02-12 DOI: 10.1016/j.jsse.2024.02.001

Paul Wilde Ph.D., P.E.

引用次数: 0

Improving air and space safety through enhanced coordination with the SpaceTracks Suite microservice architecture 通过加强与 SpaceTracks Suite 微服务架构的协调，改善航空和航天安全

Journal of Space Safety Engineering Pub Date : 2024-02-09 DOI: 10.1016/j.jsse.2024.01.005

Jens Hampe, Anouk Stahnke

{"title":"Improving air and space safety through enhanced coordination with the SpaceTracks Suite microservice architecture","authors":"Jens Hampe, Anouk Stahnke","doi":"10.1016/j.jsse.2024.01.005","DOIUrl":"10.1016/j.jsse.2024.01.005","url":null,"abstract":"<div><p>Within the SpaceTracks project, a Launch Coordination Center (LCC) prototype is currently being developed by the German Aerospace Center (DLR). The aim of the LCC is to support the coordination among stakeholders of launches and re-entries before, during, and after the operation. Thereby, interests and needs of all stakeholders should be balanced and the situational awareness should be increased. At the core of the LCC is the SpaceTracks Suite (STS) microservice architecture.</p><p>When developing software solutions to integrate spacecraft into European airspace, various aspects must be considered: different space flight characteristics, the complex air traffic system and other concept requirements like security, scalability, flexibility, resilience and arbitrarily expandability, hence an agile procedure model and a loosely coupled and flexible software design is favored. This paper describes the DLR current approach, design considerations and solution characteristics of the STS.</p></div>","PeriodicalId":37283,"journal":{"name":"Journal of Space Safety Engineering","volume":"11 1","pages":"Pages 80-86"},"PeriodicalIF":0.0,"publicationDate":"2024-02-09","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://www.sciencedirect.com/science/article/pii/S2468896724000053/pdfft?md5=50872dc90a347afa99b95ca45a6ab672&pid=1-s2.0-S2468896724000053-main.pdf","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"139876731","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"OA","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}

引用次数: 0

Design of an autonomous flight termination system for an international market with heterogeneous regulations 为法规各异的国际市场设计自主飞行终止系统

Journal of Space Safety Engineering Pub Date : 2024-02-08 DOI: 10.1016/j.jsse.2024.01.003

Julia Gente , Marc Hirth , Sven Weikert , Marc Schwarzbach , Tiago Milhano , Dimitrios Gkoutzos , Daniel Ridley , Christian Schmierer , Stephan Schuster

引用次数: 0

Improving casualty risk estimates for uncontrolled rocket body reentries 改进失控火箭箭体再入大气层的伤亡风险估计

Journal of Space Safety Engineering Pub Date : 2024-02-08 DOI: 10.1016/j.jsse.2024.01.004

Ewan Wright , Aaron Boley , Michael Byers

引用次数: 0

Comparative analytical analysis and component selection of resistojet thruster for satellite propulsion 用于卫星推进的电阻喷射推进器的比较分析和部件选择

Journal of Space Safety Engineering Pub Date : 2024-01-29 DOI: 10.1016/j.jsse.2024.01.002

Aswin M R, Akshay Pavithran, Yash Mangrole, Shriya Shivaraman, Chinmay Sanjay Kulaye, Amit Kumar Thakur, Balaji R

{"title":"Comparative analytical analysis and component selection of resistojet thruster for satellite propulsion","authors":"Aswin M R, Akshay Pavithran, Yash Mangrole, Shriya Shivaraman, Chinmay Sanjay Kulaye, Amit Kumar Thakur, Balaji R","doi":"10.1016/j.jsse.2024.01.002","DOIUrl":"https://doi.org/10.1016/j.jsse.2024.01.002","url":null,"abstract":"<div><p><span>Resistojet is a thruster<span> based on electrothermal propulsion which uses heating element to increase the temperature of the thruster, so the propellant ionizes and gives out thrust at the nozzle section. Given their high propulsive performance, resistojets are widely used in satellite technology for control, tangential orbit modification, and propulsion. Therefore, numerous experimental and numerical research was carried out to comprehend the performance of a resistojet. The four major elements of a resistojet thruster are the material for the heating element, the cooling system, the type of nozzle and the choice of propellant. The combination of these four major elements matters greatly to design an efficient resistojet thruster. The main objective here is to compare and analyze the existing high performance resistojet thrusters. Therefore, it is critical to comprehend how well the four major elements of a resistojet thruster perform under different conditions. A resistojets’ performance is greatly affected by the design of the thruster. The right choice of propellant plays an important role with respect to the performance of a resistojet thruster. Every propellant type used up to this point has been thoroughly analyzed with respect to its effect on the resistojets’ thrust and specific impulse values. Parallelly, several cooling system and flow channel designs were examined to a great extent keeping the metrics of a resistojet in mind. A thruster's nozzle is a part that enables hot gases to escape at a higher velocity. Hence, version of nozzle types was studied, and their performances are charted in this paper. In addition to the performance characteristics, future aspects of the resistojet in </span></span>electric propulsion has been discussed.</p></div>","PeriodicalId":37283,"journal":{"name":"Journal of Space Safety Engineering","volume":"11 1","pages":"Pages 20-34"},"PeriodicalIF":0.0,"publicationDate":"2024-01-29","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"139986624","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}

引用次数: 0

A study on EMI shielding in aircraft: introduction, methods and significance of using electrospun nanocomposites 飞机电磁干扰屏蔽研究：使用电纺纳米复合材料的简介、方法和意义

Journal of Space Safety Engineering Pub Date : 2024-01-13 DOI: 10.1016/j.jsse.2024.01.001

Bijulin Greety DJ, G. Jims John Wessley

{"title":"A study on EMI shielding in aircraft: introduction, methods and significance of using electrospun nanocomposites","authors":"Bijulin Greety DJ, G. Jims John Wessley","doi":"10.1016/j.jsse.2024.01.001","DOIUrl":"10.1016/j.jsse.2024.01.001","url":null,"abstract":"<div><p>In recent times, the explosion of digital appliances and radio communication systems has triggered an elevated debate over electromagnetic interference (EMI) in numerous industries, including the aerospace sector. EMI can disrupt verbal exchange systems, navigation gadgets, or even crucial flight controls. This paper aims to explore the need for EMI protection in the context of discussing the techniques and packages of nanocomposites used for effective shielding. It broadly covers the introduction to EMI shielding, strategies for effective shielding, and the utilization of advanced nanocomposites for EMI mitigation in aircraft. The paper also highlights the amplifying dependence on digital devices in the current aircraft and highlights the increasing coercion of EMI that leads to the demand for strong EMI-protecting solutions. Different EMI shielding techniques based on their effectiveness in protecting sensitive digital components from electromagnetic disturbances are discussed. The use of techniques such as EMI filters, shielded cables, and Faraday cages are investigated for applicability in distinctive aerospace appliances. The emerging requirement for slender and flexible EMI shielding materials that has resulted in the development of conductive polymer nanocomposites in recent years and the use of nanocomposites with excellent EMI shielding regardless of their sustaining mechanical properties has been discussed in detail. Different methods like in-situ polymerization, solution blending, layer-by-layer assembly, and electrospinning are also discussed. In conclusion, the importance of EMI protection in ensuring the dependable and stable operation of modern aircraft and the utility of polymer nanocomposites, a promising method to deal with EMI-related challenges in making air travel more secure and greener in the digital age has been impressed upon.</p></div>","PeriodicalId":37283,"journal":{"name":"Journal of Space Safety Engineering","volume":"11 1","pages":"Pages 150-160"},"PeriodicalIF":0.0,"publicationDate":"2024-01-13","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"139538395","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}

引用次数: 0

Tailored continuous risk management in nanosatellite space project VZLUSAT-1 using FMECA 利用 FMECA 对超小型卫星空间项目 VZLUSAT-1 进行量身定制的持续风险管理

Journal of Space Safety Engineering Pub Date : 2023-12-16 DOI: 10.1016/j.jsse.2023.11.008

Marek Cech, Martin Januska

引用次数: 0

Re‐entry safety: Analysis and plasma wind tunnel testing of spacecraft design solutions to reduce on‐ground casualty risk 重返大气层安全：航天器设计方案的分析和等离子风洞试验，以降低地面伤亡风险

Journal of Space Safety Engineering Pub Date : 2023-12-15 DOI: 10.1016/j.jsse.2023.11.014

Lucia Suriani , Antonio Caiazzo , Britta Ganzer , Tobias Lips , Patrice Laurenti , Bradley Lockett , Thorn Schleutker , Tiago Soares , James Beck

{"title":"Re‐entry safety: Analysis and plasma wind tunnel testing of spacecraft design solutions to reduce on‐ground casualty risk","authors":"Lucia Suriani , Antonio Caiazzo , Britta Ganzer , Tobias Lips , Patrice Laurenti , Bradley Lockett , Thorn Schleutker , Tiago Soares , James Beck","doi":"10.1016/j.jsse.2023.11.014","DOIUrl":"10.1016/j.jsse.2023.11.014","url":null,"abstract":"<div><p>In compliance with ISO 24,113 and ESA Space Debris Mitigation requirements, spacecrafts in Low Earth Orbit (LEO) must be removed from their operational orbit within 25 years and re-enter the Earth's atmosphere having an on-ground casualty risk lower than 1 in 10,000.</p><p><span>To maximize the number of uncontrolled re-entries, which have much less impact on system mass and costs, ESA's Clean Space initiative is investigating design for containment (D4C) techniques and collaborating with European industries and space agencies to assess, model, analyse, and test new concepts through re-entry tools and plasma wind tunnel experiments. The main objectives are to understand the </span>survivability<span> of materials and techniques suitable for different containment concepts, to improve re-entry modelling, and implement effective D4C measures.</span></p><p>This paper shows the results of these activities, that have been the first milestones in the knowledge of D4C, although further investigations are needed.</p></div>","PeriodicalId":37283,"journal":{"name":"Journal of Space Safety Engineering","volume":"11 1","pages":"Pages 52-66"},"PeriodicalIF":0.0,"publicationDate":"2023-12-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"139024381","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}

引用次数: 0

Autonomous flight termination system: The need for an international regulatory frame 自主飞行终止系统：建立国际监管框架的必要性

Journal of Space Safety Engineering Pub Date : 2023-12-08 DOI: 10.1016/j.jsse.2023.11.013

L. Miquel Parra, G. Acampa, E. Castoldi, M. Cinque, W. Dai, P. Dell'Atti, D. Caporro

引用次数: 0