Нырковский В.

Thesis for the degree of

State registration number

0496U002348

0496U002348.pdf

Date of defense

23-02-1996

Д 02.27.06

Thesis supervisor

Official opponents

Kapitanova Liudmyla Valeriivna

Analysis and Synthesis of Takeoff and Landing Performance of Transport Category Airplanes

Degtiarov Maksym Olexandrovych

Selection of rational parameters and reduction of material consumption of tail compartments of launch vehicles

Mishchenko Olexandra Vasylivna

Methodological support for the design of electrodynamic space tethered systems

Syutkina-Doronina Svetlana Vasylivna

A methodology for the optimization of design characteristics of single-stage guided rockets with solid rocket motors

Siedykh Ihor Viktorovych

The choice of design parameters of inertial means of ensuring the continuity of propellant in the tanks of the space stages of launch vehicles.