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30 search results for "procedure"
19.2.2018 Control of Validity and Assessment of Accuracy of Telemetry Results during Full-Scale Test of Launch Vehicles
2018 (2); 157-172 DOI: https://doi.org/10.33136/stma2018.02.157 Language: Russian Annotation: The measurement errors upon conducting flight tests for launch vehicles are evaluated [...]
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8.2.2018 Development of Nozzle Blocks New Manufacturing Technology without Blazing
The step-by-step sequence and procedure of research work to develop and test a new technology of cooled nozzle block manufacturing are described.
15.1.2018 The Results of Using Automated Methods to Solve Standardization Tasks in Yuzhnoye SDO Practice
Results of Using the Procedure of Terminological Monitoring for the Purpose of Normalization of Terms of International Standards in Space Sphere.
10.1.2018 The Rocket Propellant Vapors and Water Solutions Neutralization Units. The Accumulated Experience and Prospects of Updating the Neutralization Units
Procedure to Asses Compliance of Neutralization Units Characteristics with the Requirements of Environmental Regulations of Ukraine.
1.2.2016 On Minimal Aerodynamic Resistance of Rotation Body at Zero Angle of Attack in Hypersonic Non-Viscous Flow
2016 (2); 3-8 Language: Russian Annotation: To solve the problem, procedure is suggested forming the basis for two functional extremeness conditions, one of which is Euler [...]
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8.1.2019 Virtual Tests of Cassette Reentry Vehicle Dash Elements Attachment System during Ground Operation
Computational models, criteria and test procedures necessary for the analysis of the mechanical condition and prediction of the performance of the actual airframe of the [...]
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6.1.2019 Investigation into Peculiarities of Delivery to Launch Base of Rocket Propellant with Specified Gasing
In order to solve this problem number of factors have been considered, which determine the value of gas saturation in the propellants delivered to the launch site and [...]
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5.1.2019 Methodology of Normative Principles of Justification of Launch Vehicle Launching Facility Structures Lifetime
Developing strength standards and useful life calculation basis, it is advisable to use modern methods of engineering diagnostics, in particular, holographic interferometry and [...]
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3.1.2019 Analysis of Spacecraft Control Issues In Early Design Phases
Procedure of selection of the dynamic regulator parameters at the early phase of development of the control system for the orbital space plane motion about the center of mass [...]
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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 [...]
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