17.2.2018 Peculiarities of Dynamics of Recoverable Part of Stage of Aircraft-Type Configuration with Turbojet Engine

The possibility to ensure permissible overload values at the critical points of the descend trajectory and acceptable values of kinematic characteristics at the earth surface [...]

16.2.2018 Design Solutions to Prevent Propellant Ingress into SRM Case Space behind Sealing Ring

The structure was tested in the process of fueling the solid rocket motor casing and during charge polymerization. In order to comply with the specified requirements the cuff [...]

15.2.2018 Topical Issues of Creation of Space Rocket Thermostatic System Mating Points

Types and Design Features of Thermostating System Mating Points of Launch Vehicle Payload Units and Launch Vehicle and Spacecraft Bays. Experimental Investigations of [...]

14.2.2018 A Concept of Modular Transport Vehicle for Lunar Program

...Shanghai 1 Indonesia Пеканбару 1 Finland Helsinki 1 Unknown 1 France 1 Germany Falkenstein 1 Romania Voluntari 1 Netherlands Amsterdam 1 Ukraine Dnipro 1 Downloads, views [...]

13.2.2018 On an Approach to Constructing the Extremes in the Tasks of Optimal Solutions Search

Least-Time Flight Path Problem (classification of generalizations and some latest results). ...Canada Toronto; Monreale 2 Finland Helsinki 1 Philippines Bacolod City 1 [...]

12.2.2018 Methodological Support for Initial Phase Optimization of Projecting Design, Trajectory Parameters and Rocket Object Motion Control Programs

2018 (2); 101-116 DOI: https://doi.org/10.33136/stma2018.02.101 Language: Russian Annotation: The main scientific and methodological propositions for designing single-stage guided [...]

11.2.2018 Some Peculiarities of Ensuring LRE Guarantied Service Life in the Conditions of Replacement of Components of Interindustry Application

The physical ground for determining thermal ageing test modes and increased humidity test modes is set forth. The mathematical dependencies are given to determine the [...]

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17.2.2018 Peculiarities of Dynamics of Recoverable Part of Stage of Aircraft-Type Configuration with Turbojet Engine

16.2.2018 Design Solutions to Prevent Propellant Ingress into SRM Case Space behind Sealing Ring

15.2.2018 Topical Issues of Creation of Space Rocket Thermostatic System Mating Points

14.2.2018 A Concept of Modular Transport Vehicle for Lunar Program

13.2.2018 On an Approach to Constructing the Extremes in the Tasks of Optimal Solutions Search

12.2.2018 Methodological Support for Initial Phase Optimization of Projecting Design, Trajectory Parameters and Rocket Object Motion Control Programs

11.2.2018 Some Peculiarities of Ensuring LRE Guarantied Service Life in the Conditions of Replacement of Components of Interindustry Application

9.2.2018 The Impact of Worm Design on Power and Anti-Cavitation Properties of Worm-Centrifugal Pumps

8.2.2018 Development of Nozzle Blocks New Manufacturing Technology without Blazing

7.2.2018 Theoretical Models of Sound Speed Increase Effects in Gas Duct with Corrugated Wall