1960 Introduction to rocket technique. In russian book. German V-2 missiles, rockets

Hello. I traded on eBay for a long time, now I decided to try selling here on Inspire Uplift. Your attention is offered a Russian book called - "Introduction to rocket technique". Authors - Feodosyev V.I., Sinyarev G.B. The book was published in 1960, in Moscow, the State Scientific and Technical Publishing House "OBORONGIZ". Seller Notes: “Good conditiong of the book. No missing or torn pages. See foto.” Hardcover. Pages 508. Size 225 X 150 mm. The book is very much material on the German V-2 missiles. For example: 1. page 49 - there is a drawing of the internal structure of the V-2 rocket. 2. On page 52 there is a photo of a funnel formed during the fall of the V-2 rocket. 3. Page 205 - diagram of the combustion chamber of the long-range rocket engine V-2. 4. The inset between pages 438-439 shows: The plan of the cable network in quadrants and compartments of the V-2 rocket. Pneumohydraulic rocket system V-2. In addition, the book contains a lot of other information on V-2 missiles. Content: 1. Basic relations of the theory of jet propulsion.
Thrust rocket engine.
Tsiolkovsky formula for ideal rocket speed.
External efficiency of the rocket engine.
2. Types of rocket aircraft and the basics of their device.
Unmanned missile aircraft and their purpose.
Land-based rocket artillery shells short-range.
Long-range missiles.
Anti-aircraft missiles.
Other types of rocket aircraft.
Artificial satellites of the Earth and the development of interplanetary spaces.
3. Rocket engines, their device and features of work.
Energy conversion
Liquid rocket engines (LRE).
4. Fuel rocket engines.
Chemical energy of rocket engine fuels.
Modern liquid and solid fuels for rocket engines.
Nuclear reaction energy and its use in rocket engines.
5. Processes in the combustion chamber of the rocket engine.
Burning in the rocket engine.
Burning rocket powders.
Combustion products of propellant rocket engines and their properties.
Thermal dissociation and composition of combustion products.
6. The flow of combustion products through the rocket nozzle.
The basic laws of gas flow.
The flow of gas through the nozzle.
Work nozzle rocket engine.
Features of a supersonic nozzle. Characteristics of rocket engines.
Cooling liquid rocket engines.
7. Forces and moments acting on a rocket in flight.
The system of forces acting on a rocket in flight, and differential equations of motion.
Earth's atmosphere and its properties.
Aerodynamic forces.
Static and damping moments.
Governing efforts.
Changing the force of the rocket and the weight of the rocket on the path
8. The trajectory of the flight of ballistic missiles.
Trajectory sections.
Active site.
Flying outside the atmosphere in a field of earthly agony.
Loads acting on the main elements of the rocket in flight.
9. Basic principles of stabilization, control and guidance of missiles.
Ways to stabilize and control the rocket.
Gyro and its application.
Hiro devices and executive bodies of the automatic machine for the long-range missile stabilization.
Intermediate device automatic long-range missile stabilization.
Some issues of sustaining rocket flight.
Ballistic missile range control.
Electropneumatic equipment and the automatic operation of a ballistic missile at launch and in flight.
Ways of targeting guided missiles.
Dispersion when firing rockets.
10. Ground equipment, missile and rocket engine testing.
Starting systems.
Ground equipment.
Test rocket engines and rockets.                                                                           Shipment:
Item ships within 1-3 business days after the receipt of the payment.  
Usually it takes 30-40 days to Europe and 30-60 days to USA.
I send by the Russian Post with tracking number.
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