Russian Aeronautics is a journal that publishes articles on fundamental research, application, and developments in the field of aeronautical, space, rocket science and engineering that are carried out at institutes of higher education, research institutes, design bureaus, and branch enterprises. 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.
Russian Aeronautics is a peer reviewed journal. We use a single blind peer review format. Our team of reviewers includes over 50 reviewers, both internal and external (30%). The average period from submission to first decision in 2017 was 20 days, and that from first decision to acceptance was 50 days. The rejection rate for submitted manuscripts in 2017 was 5%. The final decision on the acceptance of an article for publication is made by the Editorial Board.
Any invited reviewer who feels unqualified or unable to review the manuscript due to the conflict of interests should promptly notify the editors and decline the invitation. Reviewers should formulate their statements clearly in a sound and reasoned way so that authors can use reviewer’s arguments to improve the manuscript. Personal criticism of the authors must be avoided. Reviewers should indicate in a review (i) any relevant published work that has not been cited by the authors, (ii) anything that has been reported in previous publications and not given appropriate reference or citation, (ii) any substantial similarity or overlap with any other manuscript (published or unpublished) of which they have personal knowledge.
Aircraft Production Technology
Development of a Technique to Reduce Porosity in Composite Structures at the Limited Autoclave Pressure
Flight Dynamics and Control of Flight Vehicles
Development of Algorithms for Integration and Reconfiguration of the Flight Control System and Interfaces
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