Open AccessОСОБЕННОСТИ ДИНАМИКИ ВОЗВРАЩАЕМОЙ ЧАСТИ ПЕРВОЙ СТУПЕНИ САМОЛЕТНОЙ СХЕМЫ С ТУРБОРЕАКТИВНЫМ ДВИГАТЕЛЕМ
Author(s) -
В.И. Усиченко
Publication year - 2018
Publication title -
vìsnik dnìpropetrovsʹkogo unìversitetu. serìâ: raketno-kosmìčna tehnìka
Language(s) - English
Resource type - Journals
ISSN - 2409-4056
DOI - 10.15421/451824
Subject(s) - plane (geometry) , computer science , aerospace engineering , physics , engineering , mathematics , geometry
The returned part of the first stage of plane type with a turbojet has some dynamic features. The main things from these features are reflected in this article. Possibility of reception of the landing characteristics close to the plane is estimated also.