{"title":"IAASS supports international commitments to not conduct destructive anti-satellite testing","authors":"Paul Wilde Ph.D., P.E.","doi":"10.1016/j.jsse.2024.02.001","DOIUrl":"10.1016/j.jsse.2024.02.001","url":null,"abstract":"","PeriodicalId":37283,"journal":{"name":"Journal of Space Safety Engineering","volume":null,"pages":null},"PeriodicalIF":0.0,"publicationDate":"2024-02-12","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"139812067","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}
{"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":null,"pages":null},"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}
Julia Gente , Marc Hirth , Sven Weikert , Marc Schwarzbach , Tiago Milhano , Dimitrios Gkoutzos , Daniel Ridley , Christian Schmierer , Stephan Schuster
{"title":"Design of an autonomous flight termination system for an international market with heterogeneous regulations","authors":"Julia Gente , Marc Hirth , Sven Weikert , Marc Schwarzbach , Tiago Milhano , Dimitrios Gkoutzos , Daniel Ridley , Christian Schmierer , Stephan Schuster","doi":"10.1016/j.jsse.2024.01.003","DOIUrl":"10.1016/j.jsse.2024.01.003","url":null,"abstract":"<div><p><span>Autonomous Flight Termination Systems (AFTS) are used to terminate potentially dangerous trajectories of flight vehicles and rockets before they impose an unacceptable risk to humans or assets. In the FTSnext project a system design and software prototype of an AFTS specifically for the international market of orbital microlaunchers was developed. The system design was obtained following the model-based system engineering approach. The onboard software prototype was implemented in MATLAB. Furthermore, a simulator was developed in Simulink and ASTOS to test the AFTS in nominal, failure, and near-failure trajectories. In all simulated failure trajectories, the FTSnext prototype triggers the desired termination action. The adaptability to several launchers and nominal trajectories can be shown. The performance of the core functions </span>sensor fusion and instantaneous impact point calculation were assessed with Monte Carlo simulations.</p></div>","PeriodicalId":37283,"journal":{"name":"Journal of Space Safety Engineering","volume":null,"pages":null},"PeriodicalIF":0.0,"publicationDate":"2024-02-08","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"139886311","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}
{"title":"Improving casualty risk estimates for uncontrolled rocket body reentries","authors":"Ewan Wright , Aaron Boley , Michael Byers","doi":"10.1016/j.jsse.2024.01.004","DOIUrl":"10.1016/j.jsse.2024.01.004","url":null,"abstract":"<div><p>Approximately 70 % of launches in 2022 resulted in an uncontrolled rocket body reentry<span>, creating an unnecessary casualty risk to people on the ground, at sea, and in aircraft. Rocket bodies have masses ranging from tens of kilograms to 20 tonnes. Using known rocket body masses and correlations between mass and casualty area, we present revised estimates for the expected risk, finding a 20–29 % probability of one or more casualties over the next decade.</span></p><p>Some states use a 1-in-10,000 threshold for accepting an uncontrolled reentry casualty risk when approving a space activity. This threshold, which is not universally agreed upon, represents a risk acceptance by one country, but imposed on the world population. As the use of space expands, with a record 180 successful launches in 2022, states and other launch providers should adopt technologies and mission designs that ensure controlled reentries. Uncontrolled reentries, particularly of large rocket bodies, constitute an unsafe and unnecessary practice.</p></div>","PeriodicalId":37283,"journal":{"name":"Journal of Space Safety Engineering","volume":null,"pages":null},"PeriodicalIF":0.0,"publicationDate":"2024-02-08","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"139817978","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}
{"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":"https://doi.org/10.1016/j.jsse.2024.01.005","url":null,"abstract":"","PeriodicalId":37283,"journal":{"name":"Journal of Space Safety Engineering","volume":null,"pages":null},"PeriodicalIF":0.0,"publicationDate":"2024-02-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"139816902","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}
Julia Gente, Marc Hirth, Sven Weikert, Marc Schwarzbach, Tiago Milhano, Dimitrios Gkoutzos, Daniel Ridley, Christian Schmierer, Stephan Schuster
{"title":"Design of an autonomous flight termination system for an international market with heterogeneous regulations","authors":"Julia Gente, Marc Hirth, Sven Weikert, Marc Schwarzbach, Tiago Milhano, Dimitrios Gkoutzos, Daniel Ridley, Christian Schmierer, Stephan Schuster","doi":"10.1016/j.jsse.2024.01.003","DOIUrl":"https://doi.org/10.1016/j.jsse.2024.01.003","url":null,"abstract":"","PeriodicalId":37283,"journal":{"name":"Journal of Space Safety Engineering","volume":null,"pages":null},"PeriodicalIF":0.0,"publicationDate":"2024-02-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"139826369","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}
{"title":"IAASS supports international commitments to not conduct destructive anti-satellite testing","authors":"Paul Wilde","doi":"10.1016/j.jsse.2024.02.001","DOIUrl":"https://doi.org/10.1016/j.jsse.2024.02.001","url":null,"abstract":"","PeriodicalId":37283,"journal":{"name":"Journal of Space Safety Engineering","volume":null,"pages":null},"PeriodicalIF":0.0,"publicationDate":"2024-02-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"139871862","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}
{"title":"Improving casualty risk estimates for uncontrolled rocket body reentries","authors":"E. Wright, Aaron Boley, Michael Byers","doi":"10.1016/j.jsse.2024.01.004","DOIUrl":"https://doi.org/10.1016/j.jsse.2024.01.004","url":null,"abstract":"","PeriodicalId":37283,"journal":{"name":"Journal of Space Safety Engineering","volume":null,"pages":null},"PeriodicalIF":0.0,"publicationDate":"2024-02-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"139877568","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}
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":null,"pages":null},"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}
{"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":null,"pages":null},"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}