2.2.2025 Performance analysis and validation of a monopropellant air-detonation ramjet engine

Experimental study on the rotating detonation engine based on a gas mixture.

3.1.2025 Experimental research on separation diaphragm performance in propellant storage and feed systems of liquid propellant tanks

The relevance of this study arises from the need to ensure the reliable separation of gas and liquid duringthe operation of aerospace systems under diff erent [...]

2.1.2024 New and advanced liquid rocket engines of the Yuzhnoye SDO

Over the past 66 years Yuzhnoye SDO has developed more than 40 liquid rocket engines (LRE) of various purpose, designed both to gas-generator cycle and to staged combustion [...]

2.1.2020 Analysis of development trends of design parameters and basic characteristics of missiles for the advanced multiple launch rocket systems

Gasodinamika porokhovykh raketnykh dvigatelei: inzhenernye metody rascheta.

12.1.2024 Hardening of steels modifying their surfaces with ion-plasma nitriding in glow discharge

Hydrogen was added to the argon-nitrogen gaseous medium to intensify the nitriding process. The choice of the optimal temperature and time parameters of gas nitriding [...]

8.1.2024 Theoretic-experimental evaluation of the solid-propellant grain erosive burning

Gas flow rate in each interval of the grain channel is calculated using gas-dynamic equations. Gasodynamicheskie funktsii. Content 2024 (1) Downloads: 237 [...]

15.1.2024 Enhancing operability of the fuel system units in the hot climate conditions

Heat resistance during compression is most important for rubbers used for seals of various types: rings, collars, armored collars, gaskets for aviation and rocket technology [...]

7.1.2024 Selection of the functional units for the Cyclone-4M ILV separation system

Brief characteristics of these systems are given, based on the gas-reactive nozzle thrust, braking with solid-propellant rocket engines, separating with spring or pneumatic [...]

10.1.2020 Calculation and selection of parameters for a propellant consumption diagram of dual-thrust main SRM

Gasotermodinamika raketnykh dvigatelei na tverdom toplive.

3.1.2020 Analysis of the unsteady stress-strain behavior of the launch vehicle hold-down bay at liftoff

Stress and deformation of rocket gas turbine disc under different loads using finite element modeling.