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

BURN RATE AUGMENTATION OF COMPOSITE PROPELLANT ADJACENT TO INSULATION MATERIALS

卷 13, 册 1, 2014, pp. 65-81
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2014005355
Get accessGet access

摘要

Bristol manufactures several small solid propellant rocket motors using a composite HTPB/AP based propellant system. Most Bristol rocket motors developed prior to 1990 used an internal insulation system consisting of an asbestos-filled roll-form butadiene (RF/B) case insulation material, with an aluminum liner between the propellant and the insulation. Due to health and safety regulations, processing of asbestos containing insulation materials is no longer permissible. The RF/B insulation system has been replaced with alternate insulation systems which use a Bristol proprietary carbon-filled (CF/P) liner to interface with the propellant. The CF/P liner uses the same polymer system as the propellant, and provides limited insulating capabilities as well as promoting case bonding of the propellant. Motors using the CF/P liner system have shown an augmentation in the propellant burning rate prior to motor tail-off compared to their previous RF/B insulated versions. The performance changes are attributed to a localized augmentation of the propellant burning rate adjacent to the CF/P liner interface. This paper will discuss potential mechanisms for the burning rate augmentation effect, and describes the results of testing and analyses performed to evaluate the phenomenon.

参考文献
  1. Giants, T.W. , Case bond liner systems for solid rocket motors.

  2. Gossant, B. , Solid propellant combustion and internal ballistics of motors, In Davenas A., Solid Rocket Propulsion Technology.

  3. Libardi, J., Ravagnani, S. P., Morais, A. M. F., and Cardoso, A. R. , Study of plasticizer diffusion in a solid rocket motor's bondline.

665 文章浏览量 50 文章下载 统计数据
665 文章浏览量 50 下载次数 Google
Scholar
引用次数

相似内容的文章:

DIAGNOSTIC TOOLS FOR STUDIES ON BURN-RATE BEHAVIOR OF ADVANCED SOLID PROPELLANTS International Journal of Energetic Materials and Chemical Propulsion, Vol.3, 1994, issue 1-6
A. N. Nazare, S. S. Dhar, Haridwar Singh, SHRINANDAN ASTHANA, P. G. Shrotri
ENHANCEMENT OF COMPOSITE PROPELLANT IGNITION CHARACTERISTICS BY SURFACE ABRASION International Journal of Energetic Materials and Chemical Propulsion, Vol.12, 2013, issue 4
Jacquie Hewson , Robert Le Neal
IGNITION AND COMBUSTION CHARACTERISTICS OF A MICRO-ELECTROMECHANICAL SYSTEM (MEMS) PYROTECHNIC THRUSTER FOR MICRO PROPULSION APPLICATIONS International Journal of Energetic Materials and Chemical Propulsion, Vol.16, 2017, issue 2
Harshit Shukla, Mohan Varma, Gusain Rajesh Singh Nandan, Vinod Kumar, Priyanka Shukla
IGNITION OF LIQUID AND SOLID NITROCOMPOUNDS AT FAST COMPRESSION OF GAS INTRUSIONS International Journal of Energetic Materials and Chemical Propulsion, Vol.4, 1997, issue 1-6
E. L. Dorofeev, Yu. N. Polikarpov, B. N. Kondrikov
TOWARD HIGH-PERFORMANCE, GREENER, AND LOW-VULNERABILITY MUNITIONS WITH THE RIGHTTRAC TECHNOLOGY DEMONSTRATOR PROGRAM International Journal of Energetic Materials and Chemical Propulsion, Vol.13, 2014, issue 1
Patrick Brousseau, Fanny Monteil-Rivera, Sylvie Rocheleau, Geoffrey I. Sunahara, Sebastien Cote, F. Cote, Jalal Hawari, Sylvie Brochu, M. Brassard, I. Poulin, Emmanuela Diaz, Richard Martel, Guy Ampleman, Catalin Florin Petre, Sonia Thiboutot
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