Basics of design of rocket-directional engines
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The training manual sets out the thermo-aerodynamic basics of designing rocket-directional engines (RPD) for unmanned aerial vehicles . Considerable attention is paid to the integrated design of the RAP, including engineering methods for calculating output characteristics, and the choice of fuel type, as well as determining the optimal characteristics of the aircraft and automatic control systems. The proposed methods for calculating the optimal parameters of the aircraft, RAP and automatic control systems provide the maximum flight range .
LF/213530710/R
Data sheet
- Name of the Author
- Мазинг Г.Ю.
Орлов Б.В.
Рейдел А.Л.
Степанов М.Н.
Топчеев Ю.И. - Language
- Russian
- Release date
- 1967
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The training manual sets out the thermo-aerodynamic basics of designing rocket-directional engines (RPD) for unmanned aerial vehicles . Considerable attention i...