Development of LM10-MIRA LOX/LNG expander cycle demonstrator engine
| Autor: | Paolo Bellomi, Rocco Pellegrini, Mikhail Rudnykh, Luigi Arione, Stefano Carapellese, V. S. Rachuk, Emanuela D’Aversa, A.A. Gurtovoy, Giuseppe Caggiano, Daniele Liuzzi, S.D. Lobov |
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| Rok vydání: | 2016 |
| Předmět: |
020301 aerospace & aeronautics
Engineering business.product_category business.industry Vega Aerospace Engineering Thrust 02 engineering and technology 01 natural sciences 010305 fluids & plasmas 0203 mechanical engineering Aeronautics Rocket 0103 physical sciences business Third stage Liquefied natural gas |
| Zdroj: | Acta Astronautica. 126:364-374 |
| ISSN: | 0094-5765 |
| DOI: | 10.1016/j.actaastro.2016.04.018 |
| Popis: | 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). |
| Databáze: | OpenAIRE |
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