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47 search results for "gas"
10.2.2016 Mathematical Model of High-Flowrate Electropneumatic Valve
2016 (2); 65-71 Language: Russian Annotation: The developed mathematical model of electropneumatic valve, taking into account gas flow inertia in pneumatic pipelines, is [...]
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7.1.2019 Experience of Development and Use of Generator Pressurization System for Tanks of Launch Vehicles on High-Temperature Propellants
Replacement of gas bottle pressurization systems with generating ones on such launch vehicles as 15A14, 15A15, 11K68 (8K67), 15A18M substantially simplified operation, [...]
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21.1.2019 Optimization of Geometrical Shape of Isolation Valve Blading Position
It results in the decrease of the required pressurization gas volume, which boosts reduction of the performance of the launch vehicle as a whole.
17.1.2019 Development of Prospective Small-Size Auxiliary SMR of New Type
2019, (1); 114-121 DOI: https://doi.org/10.33136/stma2019.01.114 Language: Russian Annotation: This article considers essentially new versions of small-sized solid propellant rocket [...]
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7.1.2023 Specificity of using rubbers as structural materials for making connector assemblies of temperature conditioning systems
For separation systems with increased requirements to external actions and cleanliness, authors developed a shear explosive bolt or pyrobolt, divided into parts, cutting the body [...]
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5.1.2023 Fueling-neutralization stations. New developments and applications
Key words: saturation with helium and denitrogenation of the propellant , drain with closed vent device , excessive pressure draining , gas-vapor mixture , neutralization [...]
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3.1.2023 Analysis of a modernized 9K51 Hrad Multiple Rocket Launcher System to determine the performance specifications of the 122-mm unguided rocket projectile in development
Oskolochno-fugasniy snaryad 9M521. Tablitsy strelby oskolochno-fugasnymi snaryadami M-21OF. 9M521.122-mm neupravlyaemiy oskolochno-fugasniy reaktivniy snaryad s [...]
Read more 3.1.2023 Analysis of a modernized 9K51 Hrad Multiple Rocket Launcher System to determine the performance specifications of the 122-mm unguided rocket projectile in development