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221 search results for "test load"
19.1.2019 Peculiarities of Radio Transparent Fairings Development
...Kyiv; Dnipro; Kyiv 5 Cambodia Phnom Penh 1 Finland Helsinki 1 Unknown 1 Canada Monreale 1 Germany Falkenstein 1 Romania Voluntari 1 Netherlands Amsterdam 1 Downloads, [...]
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18.1.2019 Designing of Servo Driver of Throttle Mechanisms and Fuel Flow Regulator of ILV Main Motor
Functional mockups of the executive unit, control box, as well as the computer-controlled technological test console were manufactured on the basis of the requirements [...]
Read more 18.1.2019 Designing of Servo Driver of Throttle Mechanisms and Fuel Flow Regulator of ILV Main Motor
17.1.2019 Development of Prospective Small-Size Auxiliary SMR of New Type
Testing SRE with pyroxiline powder grain showed that the optimum design of the engine can be developed only with the application of the specially developed design procedure [...]
Read more 17.1.2019 Development of Prospective Small-Size Auxiliary SMR of New Type
16.1.2019 Oscillation Processes in Rig at the Moment of SRM Transfer to Main Operation Mode
2019, (1); 110-113 DOI: https://doi.org/10.33136/stma2019.01.110 Language: Ukrainian Annotation: This paper describes the configuration of the rig, designed to fasten the [...]
Read more 16.1.2019 Oscillation Processes in Rig at the Moment of SRM Transfer to Main Operation Mode
14.1.2019 Technique of Determination of SRM Operational Life Taking into Account Materials and Elements Strength Margins
Strength properties of the material should be reduced to test conditions in terms of temperature, pressure, rate of loading, degrees of material aging etc.
13.1.2019 Prediction of Solid Propellant Burnout Time in Launch Vehicle Propulsion System in Flight
Based on the statistical processing of the deviations of the predicted time of solid fuel burn-out versus the realized one it was determined that the forecast based on the results [...]
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12.1.2019 Monitoring of Launch Platform Drift Parameters during Zenit-3SL Integrated Launch Vehicle Prelauch Processing
To ensure the payload orbiting accuracy the following maximum permissible values of platform drift parametres were determined: • These values during prelaunch processing of [...]
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21.1.2016 Selection of Optimal Parameters of Wind Desalting System with Hydrogen Energy Storage Unit
...Dnipro; Dnipro 2 Cambodia Phnom Penh 1 Finland Helsinki 1 France 1 Canada Monreale 1 Germany Falkenstein 1 Romania Voluntari 1 Netherlands Amsterdam 1 Unknown 1 Downloads, [...]
Read more 21.1.2016 Selection of Optimal Parameters of Wind Desalting System with Hydrogen Energy Storage Unit
20.1.2016 Determination of External Characteristic of Autonomous WPP for Regulation by Rotor Withdrawal from under Wind
2016 (1); 122-127 Language: Russian Annotation: The procedure and program were developed for calculation of rotor external characteristic (rotor rotation frequency as a function of [...]
Read more 20.1.2016 Determination of External Characteristic of Autonomous WPP for Regulation by Rotor Withdrawal from under Wind
19.1.2016 Blade Geometry for Maximal Power Coefficient and Minimal Noise Level
...Dnipro 2 Cambodia Phnom Penh 1 Finland Helsinki 1 Great Britain London 1 Canada Monreale 1 Germany Falkenstein 1 Romania Voluntari 1 Netherlands Amsterdam 1 Downloads, [...]
Read more 19.1.2016 Blade Geometry for Maximal Power Coefficient and Minimal Noise Level