10.2.2016 Mathematical Model of High-Flowrate Electropneumatic Valve

High convergence of test data with calculation results is obtained, making it possible to apply the developed mathematical model for evaluation of transient parameters, when [...]

Read more 10.2.2016 Mathematical Model of High-Flowrate Electropneumatic Valve

8.2.2016 Development and Validation of Program Module for Construction of Virtual Models of Real Structures in ANSYS System

...Singapore; Singapore; Singapore 6 Unknown Padstow; 2 Ukraine Dnipro; Dnipro 2 Finland Helsinki 1 Canada Monreale 1 Germany Falkenstein 1 Romania Voluntari 1 Downloads, [...]

Read more 8.2.2016 Development and Validation of Program Module for Construction of Virtual Models of Real Structures in ANSYS System

7.2.2016 Analysis of Operation Modes and Selection of Chemical Current Source Included in Autonomous Electric Power Supply Systems of Self-Propelled Launcher

...Singapore; Singapore; Singapore; Singapore 6 Ukraine Dnipro; Dnipro 2 Finland Helsinki 1 Unknown 1 Canada Monreale 1 Germany Falkenstein 1 Romania Voluntari 1 Downloads, [...]

Read more 7.2.2016 Analysis of Operation Modes and Selection of Chemical Current Source Included in Autonomous Electric Power Supply Systems of Self-Propelled Launcher

4.2.2016 Experimental Investigations of Possibility of Creating Impulse SRM with Short Operation Period

The tests of prototype motor show the development capability of such motor. ...Singapore; Singapore 5 Germany ; Falkenstein 2 Ukraine Dnipro; Dnipro 2 Finland Helsinki 1 [...]

Read more 4.2.2016 Experimental Investigations of Possibility of Creating Impulse SRM with Short Operation Period

3.2.2016 Selection of Optimal Trajectories of Spacecraft Launch Vehicles

Content 2016 (2) Downloads: 38 Abstract views: 508 Dynamics of article downloads Dynamics of abstract views Downloads geography Country City Downloads [...]

Read more 3.2.2016 Selection of Optimal Trajectories of Spacecraft Launch Vehicles

9.1.2019 Modeling of Cyclone-4M Rocket Jet Acoustic Emission by Volumetric Source

Therewith, the loads can be created that are critical for the launching equipment, rocket body and especially for the spacecraft, which are under the fairing. The maximal [...]

Read more 9.1.2019 Modeling of Cyclone-4M Rocket Jet Acoustic Emission by Volumetric Source

7.1.2019 Experience of Development and Use of Generator Pressurization System for Tanks of Launch Vehicles on High-Temperature Propellants

2019, (1); 45-53 DOI: https://doi.org/10.33136/stma2019.01.045 Language: Russian Annotation: Long-term experience in development, development testing and use of generating [...]

Read more 7.1.2019 Experience of Development and Use of Generator Pressurization System for Tanks of Launch Vehicles on High-Temperature Propellants

6.1.2019 Investigation into Peculiarities of Delivery to Launch Base of Rocket Propellant with Specified Gasing

...4 Germany ; Falkenstein 2 Ukraine Zaporizhia; Dnipro 2 Unknown Melbourne 1 Finland Helsinki 1 Canada Monreale 1 Romania Voluntari 1 Netherlands Amsterdam 1 Downloads, [...]

Read more 6.1.2019 Investigation into Peculiarities of Delivery to Launch Base of Rocket Propellant with Specified Gasing

5.1.2019 Methodology of Normative Principles of Justification of Launch Vehicle Launching Facility Structures Lifetime

Service limit of launch site is suggested to be the critical time or the number of cycles (launches) over this period, after which the specified limiting states are achieved in the [...]

Read more 5.1.2019 Methodology of Normative Principles of Justification of Launch Vehicle Launching Facility Structures Lifetime

4.1.2019 Mathematic Modeling and Investigation into Stress-Strain State of Space Rocket Bays

Key words: sandwich structure , interstage bay , finite-element model , manufacturing deviations , test loads Bibliography: 1. sandwich structure , interstage bay , [...]

Read more 4.1.2019 Mathematic Modeling and Investigation into Stress-Strain State of Space Rocket Bays