{"title":"空间运载火箭的能效优化评价","authors":"C. White, Jeffrey E. Dyas, Bryan L. Mesmer","doi":"10.2514/1.i011241","DOIUrl":null,"url":null,"abstract":"Space launch vehicles are highly complex multidisciplinary systems with multiple subsystems. These subsystems vary significantly, complicating the selection of an objective function. Exergy efficiency has been suggested by some as a suitable objective function with relevance across a diverse set of subsystems; however, some characteristics of exergy efficiency may make it poorly suited for the task. At its core, exergy is the amount of work available from a system for a certain environment. In this paper, the use of exergy efficiency in the optimization of a space launch vehicle is explored. Exergy efficiency objective functions are constructed, including and excluding mass decreases from staging. These objective functions are used for the optimization of a physics-based rocket trajectory model. The results are compared to historical Saturn V data and analyzed to investigate the suitability of the metric. Due to the importance of mass in mechanical energy calculations, exergy efficiency can favor designs with more massive final stages, particularly when calculations include the staging-related mass decreases.","PeriodicalId":50260,"journal":{"name":"Journal of Aerospace Information Systems","volume":"5 1","pages":""},"PeriodicalIF":1.3000,"publicationDate":"2023-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Evaluation of Exergy Efficiency Optimization of Space Launch Vehicles\",\"authors\":\"C. White, Jeffrey E. Dyas, Bryan L. Mesmer\",\"doi\":\"10.2514/1.i011241\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Space launch vehicles are highly complex multidisciplinary systems with multiple subsystems. These subsystems vary significantly, complicating the selection of an objective function. Exergy efficiency has been suggested by some as a suitable objective function with relevance across a diverse set of subsystems; however, some characteristics of exergy efficiency may make it poorly suited for the task. At its core, exergy is the amount of work available from a system for a certain environment. In this paper, the use of exergy efficiency in the optimization of a space launch vehicle is explored. Exergy efficiency objective functions are constructed, including and excluding mass decreases from staging. These objective functions are used for the optimization of a physics-based rocket trajectory model. The results are compared to historical Saturn V data and analyzed to investigate the suitability of the metric. Due to the importance of mass in mechanical energy calculations, exergy efficiency can favor designs with more massive final stages, particularly when calculations include the staging-related mass decreases.\",\"PeriodicalId\":50260,\"journal\":{\"name\":\"Journal of Aerospace Information Systems\",\"volume\":\"5 1\",\"pages\":\"\"},\"PeriodicalIF\":1.3000,\"publicationDate\":\"2023-07-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Journal of Aerospace Information Systems\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://doi.org/10.2514/1.i011241\",\"RegionNum\":4,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q2\",\"JCRName\":\"ENGINEERING, AEROSPACE\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Journal of Aerospace Information Systems","FirstCategoryId":"5","ListUrlMain":"https://doi.org/10.2514/1.i011241","RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
Evaluation of Exergy Efficiency Optimization of Space Launch Vehicles
Space launch vehicles are highly complex multidisciplinary systems with multiple subsystems. These subsystems vary significantly, complicating the selection of an objective function. Exergy efficiency has been suggested by some as a suitable objective function with relevance across a diverse set of subsystems; however, some characteristics of exergy efficiency may make it poorly suited for the task. At its core, exergy is the amount of work available from a system for a certain environment. In this paper, the use of exergy efficiency in the optimization of a space launch vehicle is explored. Exergy efficiency objective functions are constructed, including and excluding mass decreases from staging. These objective functions are used for the optimization of a physics-based rocket trajectory model. The results are compared to historical Saturn V data and analyzed to investigate the suitability of the metric. Due to the importance of mass in mechanical energy calculations, exergy efficiency can favor designs with more massive final stages, particularly when calculations include the staging-related mass decreases.
期刊介绍:
This Journal is devoted to the dissemination of original archival research papers describing new theoretical developments, novel applications, and case studies regarding advances in aerospace computing, information, and networks and communication systems that address aerospace-specific issues. Issues related to signal processing, electromagnetics, antenna theory, and the basic networking hardware transmission technologies of a network are not within the scope of this journal. Topics include aerospace systems and software engineering; verification and validation of embedded systems; the field known as ‘big data,’ data analytics, machine learning, and knowledge management for aerospace systems; human-automation interaction and systems health management for aerospace systems. Applications of autonomous systems, systems engineering principles, and safety and mission assurance are of particular interest. The Journal also features Technical Notes that discuss particular technical innovations or applications in the topics described above. Papers are also sought that rigorously review the results of recent research developments. In addition to original research papers and reviews, the journal publishes articles that review books, conferences, social media, and new educational modes applicable to the scope of the Journal.