ОСОБЕННОСТИ ДИНАМИКИ ВОЗВРАЩАЕМОЙ ЧАСТИ ПЕРВОЙ СТУПЕНИ САМОЛЕТНОЙ СХЕМЫ С ТУРБОРЕАКТИВНЫМ ДВИГАТЕЛЕМ
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.
2018 ◽
Vol 6
(8)
◽
pp. 58
2020 ◽
pp. 62-67
Keyword(s):
Keyword(s):
2011 ◽
Vol 704-705
◽
pp. 352-357