图书馆订阅: Guest
国际能源材料和化学驱动期刊

每年出版 6 

ISSN 打印: 2150-766X

ISSN 在线: 2150-7678

The Impact Factor measures the average number of citations received in a particular year by papers published in the journal during the two preceding years. 2017 Journal Citation Reports (Clarivate Analytics, 2018) IF: 0.7 To calculate the five year Impact Factor, citations are counted in 2017 to the previous five years and divided by the source items published in the previous five years. 2017 Journal Citation Reports (Clarivate Analytics, 2018) 5-Year IF: 0.7 The Immediacy Index is the average number of times an article is cited in the year it is published. The journal Immediacy Index indicates how quickly articles in a journal are cited. Immediacy Index: 0.1 The Eigenfactor score, developed by Jevin West and Carl Bergstrom at the University of Washington, is a rating of the total importance of a scientific journal. Journals are rated according to the number of incoming citations, with citations from highly ranked journals weighted to make a larger contribution to the eigenfactor than those from poorly ranked journals. Eigenfactor: 0.00016 The Journal Citation Indicator (JCI) is a single measurement of the field-normalized citation impact of journals in the Web of Science Core Collection across disciplines. The key words here are that the metric is normalized and cross-disciplinary. JCI: 0.18 SJR: 0.313 SNIP: 0.6 CiteScore™:: 1.6 H-Index: 16

Indexed in

OVERVIEW OF BORON DUCTED ROCKET DEVELOPMENT

卷 2, 册 1-6, 1993, pp. 133-178
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v2.i1-6.60
Get accessGet access

摘要

The paper summarizes technological and project oriented development work carried out at MBB and Bayern-Chemie since 1970. The objective of the work was to develop propulsion systems far superior to conventional rocket motors to be applied for long range surface/surface or surface/air missions. Ultimate performance and reliability requirements led to the ducted rocket using high energy solid propellants. Highly boron loaded propellant formulations promise a most favourable energetic potential. However the combustion characteristics of boron impose numerous problems requiring closely integrated development work for propellant formulation and engine design. The paper is subdivided into
1. propellant development
2. engine development and design
3. development testing and results
The first two paragraphs are looking at those fields where the propulsion system development is especially challenged by the application of boron. Emphasis is laid on the illustration of the close interrelationship between solutions to be found for propellant and/or engine related problems.
The third paragraph gives an overview of the technical level which has been achieved with the boron ducted rocket and examples of the application to various propulsion systems developed at MBB/Bayern-Chemie.

对本文的引用
  1. Jung Woosuk, Jung Sangwoo, Kwon Taesoo, Park Juhyeon, Kwon Sejin, Ignition Delay in Solid-Fuel Ramjet Combustor, Journal of Propulsion and Power, 34, 6, 2018. Crossref

  2. Jung Woosuk, Baek Seungkwan, Park Juhyeon, Kwon Sejin, Combustion Characteristics of Ramjet Fuel Grains with Boron and Aluminum Additives, Journal of Propulsion and Power, 34, 4, 2018. Crossref

  3. GUO Yang, ZHANG Wei, ZHOU Xing, DENG Lei, Oxidation Characteristics of Magnesium Diboride, Journal of Inorganic Materials, 34, 8, 2019. Crossref

  4. Hashim Syed Alay, Lahariya Manu, Karmakar Srinibas, Roy Arnab, Calculation of Theoretical Performance of Boron-Based Composite Solid Propellant for the Future Applications, in Innovative Design and Development Practices in Aerospace and Automotive Engineering, 2017. Crossref

  5. Liu Daoping, Xia Zhixun, Huang Liya, Hu Jianxin, Boron Particle Combustion in Solid Rocket Ramjets, Journal of Aerospace Engineering, 28, 4, 2015. Crossref

Begell Digital Portal Begell 数字图书馆 电子图书 期刊 参考文献及会议录 研究收集 订购及政策 Begell House 联系我们 Language English 中文 Русский Português German French Spain