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Feasibility Study and Demonstration of an Aluminum and Ice Solid Propellant
المؤلفون المشاركون
Tsohas, John
Pfeil, Mark A.
Pourpoint, Timothee L.
Son, Steven F.
Wood, Tyler D.
المصدر
International Journal of Aerospace Engineering
العدد
المجلد 2012، العدد 2012 (31 ديسمبر/كانون الأول 2012)، ص ص. 1-11، 11ص.
الناشر
Hindawi Publishing Corporation
تاريخ النشر
2012-07-18
دولة النشر
مصر
عدد الصفحات
11
التخصصات الرئيسية
العلوم الهندسية و تكنولوجيا المعلومات
الملخص EN
Aluminum-water reactions have been proposed and studied for several decades for underwater propulsion systems and applications requiring hydrogen generation.
Aluminum and water have also been proposed as a frozen propellant, and there have been proposals for other refrigerated propellants that could be mixed, frozen in situ, and used as solid propellants.
However, little work has been done to determine the feasibility of these concepts.
With the recent availability of nanoscale aluminum, a simple binary formulation with water is now feasible.
Nanosized aluminum has a lower ignition temperature than micron-sized aluminum particles, partly due to its high surface area, and burning times are much faster than micron aluminum.
Frozen nanoscale aluminum and water mixtures are stable, as well as insensitive to electrostatic discharge, impact, and shock.
Here we report a study of the feasibility of an nAl-ice propellant in small-scale rocket experiments.
The focus here is not to develop an optimized propellant; however improved formulations are possible.
Several static motor experiments have been conducted, including using a flight-weight casing.
The flight weight casing was used in the first sounding rocket test of an aluminum-ice propellant, establishing a proof of concept for simple propellant mixtures making use of nanoscale particles.
نمط استشهاد جمعية علماء النفس الأمريكية (APA)
Pourpoint, Timothee L.& Wood, Tyler D.& Pfeil, Mark A.& Tsohas, John& Son, Steven F.. 2012. Feasibility Study and Demonstration of an Aluminum and Ice Solid Propellant. International Journal of Aerospace Engineering،Vol. 2012, no. 2012, pp.1-11.
https://search.emarefa.net/detail/BIM-505255
نمط استشهاد الجمعية الأمريكية للغات الحديثة (MLA)
Pourpoint, Timothee L.…[et al.]. Feasibility Study and Demonstration of an Aluminum and Ice Solid Propellant. International Journal of Aerospace Engineering No. 2012 (2012), pp.1-11.
https://search.emarefa.net/detail/BIM-505255
نمط استشهاد الجمعية الطبية الأمريكية (AMA)
Pourpoint, Timothee L.& Wood, Tyler D.& Pfeil, Mark A.& Tsohas, John& Son, Steven F.. Feasibility Study and Demonstration of an Aluminum and Ice Solid Propellant. International Journal of Aerospace Engineering. 2012. Vol. 2012, no. 2012, pp.1-11.
https://search.emarefa.net/detail/BIM-505255
نوع البيانات
مقالات
لغة النص
الإنجليزية
الملاحظات
Includes bibliographical references
رقم السجل
BIM-505255
قاعدة معامل التأثير والاستشهادات المرجعية العربي "ارسيف Arcif"
أضخم قاعدة بيانات عربية للاستشهادات المرجعية للمجلات العلمية المحكمة الصادرة في العالم العربي
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