Аuthors
Kuprikov M. Y.1*,
Komissarov A. A.,
Roy R. I.2**
1. ,
2. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
*e-mail: kuprikov@mai.ru
**e-mail: romaroy@rambler.ru
Abstract
This article is dedicated to the peculiarities of the maneuverable aircraft face design process under the cost limitation conditions.
It shows the importance of the aircraft cost definition at the earlier stages of design process, ways of radio cross section lowering
and their connection with parameters that determine its cost. The inverse task of design is shown in the area of the radar-tracking
visibility.
Keywords:
design; mass; cost; airframe; parameter; radar-tracking visibility level.