2.2.2018 Yuzhnoye SDO-Developed Upper Stage Liquid Rocket Engines

2018 (2); 8-15 DOI: https://doi.org/10.33136/stma2018.02.008 Language: Russian Annotation: One of the important directions in the development of Yuzhnoye SDO liquid rocket engines [...]

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13.1.2018 On Selection of Materials for Creation of Modern LV Thermostating System Mating Hoses

2 Organization: Yangel Yuzhnoye State Design Office, Dnipro, Ukraine 1 ; State Enterprise DINTEM Ukrainian Research Design-Technological Institute of Elastomer Materials and [...]

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2.1.2018 Dehydration of Hydrocarbon Fuels by Method of Over-Saturation Drop

A comparison of nitrogen and time specific consumption in dehydration operations is done and recommendations are given for their use in the cosmodromes’ launch complexes fuel [...]

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18.2.2017 Development Test of Payload Fairing Separation Dynamics under Ground Conditions

Fundamentals of Spacecraft Launch Vehicles Designing / Under the editorship of V. ...Downloads: 46 Abstract views: 337 Dynamics of article downloads Dynamics of abstract [...]

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17.2.2017 Development Test of Spacecraft Separation Dynamics under Ground Conditions

Fundamentals of Spacecraft Launch Vehicle Designing / Under the editorship of V. ...2) Downloads: 41 Abstract views: 540 Dynamics of article downloads Dynamics of abstract [...]

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12.2.2017 Determination Procedure for Pneudraulic System and Its Components No-Failure Operation Probability

2017 (2); 60-64 Language: Russian Annotation: The calculation procedure is proposed, the analysis is made and the ranges of optimal probability values of no-failure operation of [...]

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8.2.2017 Analysis Method of Nitrogen Tetroxide Tanks Generating Pressurization Systems

Launch Vehicle Propellant Tanks Pressurization Systems. Content 2017 (2) Downloads: 31 Abstract views: 299 Dynamics of article downloads Dynamics of abstract views Downloads [...]

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8.1.2017 Initial Imperfection Effect on Loss of Rod Stability under Axial Compression Conditions

On Physical Substantiation of Spontaneous Change of Initial Shape of Extremely Compressed Launch Vehicle Bays. On Prediction of Destruction of Extremely Compressed [...]

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6.2.2016 Experimental Investigations into Results of Testing Cyclone-4 ILV Thermostating System Mating Points

2 Organization: Yangel Yuzhnoye State Design Office, Dnipro, Ukraine 1 ; State Enterprise DINTEM Ukrainian Research Design-Technological Institute of Elastomer Materials and [...]

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

2019, (1); 64-71 DOI: https://doi.org/10.33136/stma2019.01.064 Language: Russian Annotation: During lift-off of integrated launch vehicles, the propulsion system jet [...]

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