Publisher: Allerton Press, Inc.
ISSN PRINT: 1068-7998
ISSN ONLINE: 1934-7901
Authors will have the option to choose how their article is published.
Traditional publishing model: published articles are made available to institutions and individuals who subscribe to this journal or who pay to read specific articles. There is no charge to publish.
Open Access (OA) model: published articles are freely and permanently available online. Anyone, anywhere can read and build upon this research. If you would be interested in publishing Open Access in this journal please follow the link.
Russian Aeronautics is a peer-reviewed journal that publishes articles addressing fundamental research, applications, and advancements within the domains of aeronautics, space exploration, rocket science, and engineering. These contributions emanate from academic institutions, research institutes, design bureaus, and research and development units. Subjects covered in the journal are aircraft and rocket equipment design; aerodynamics, strength, dynamics, and control of flight vehicles; aircraft and rocket engine theory and design; technology, automation of aircraft/rocket equipment design and production; aircraft instruments and instrumentation computer complexes. The journal welcomes manuscripts from all countries. The journal covers a wide range of subjects, including the design of aircraft and rocket equipment, aerodynamics, structural integrity, dynamics, flight vehicle control; the theory and design of aircraft and rocket engines; technological aspects and automation involved in the design and production of aircraft and rocket equipment; and aircraft instrumentation and related computational units. The journal has the aim to become an international publication and publishes manuscripts originally submitted in English from all countries along with translated works.
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Queries about submission issues, peer review process, or the status of your manuscript should be sent to the Editorial Office of Russian Aeronautics: rusaero@pleiadesonline.com
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