کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
8056159 1519928 2016 11 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Development of LM10-MIRA LOX/LNG expander cycle demonstrator engine
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی هوافضا
پیش نمایش صفحه اول مقاله
Development of LM10-MIRA LOX/LNG expander cycle demonstrator engine
چکیده انگلیسی
This article contains results of joint works by Konstruktorskoe Buro Khimavtomatiki (KBKhA, Russia) and AVIO Company (Italy) on creation of the LM10-MIRA liquid-propellant rocket demonstrator engine for the third stage of the upgraded “Vega” launcher.Scientific and research activities conducted by KBKhA and AVIO in 2007-2014 in the frame of the LYRA Program, funded by the Italian Space Agency, with ELV as Prime contractor, and under dedicated ASI-Roscosmos inter-agencies agreement, were aimed at development and testing of a 7.5 t thrust expander cycle demonstrator engine propelled by oxygen and liquid natural gas (further referred to as LNG).
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Acta Astronautica - Volume 126, September–October 2016, Pages 364-374
نویسندگان
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