7.1.2024 Selection of the functional units for the Cyclone-4M ILV separation system

pneumatic pusher , spring pusher , SPRE , gas-reactive nozzles , Zenit LV , Dnepr LV , Falcon 9 rocket , Cyclone-4М LV. pneumatic pusher , spring pusher [...]

Read more 7.1.2024 Selection of the functional units for the Cyclone-4M ILV separation system

12.1.2019 Monitoring of Launch Platform Drift Parameters during Zenit-3SL Integrated Launch Vehicle Prelauch Processing

2019, (1); 81-86 DOI: https://doi.org/10.33136/stma2019.01.082 Language: Russian Annotation: Under the Sea Launch program when developer of the Zenit-3SL ILV control [...]

Read more 12.1.2019 Monitoring of Launch Platform Drift Parameters during Zenit-3SL Integrated Launch Vehicle Prelauch Processing

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

Zenit-2. URL: https://ru.wikipedia.org/wiki/Zenit-2_(launch vehicle) . Zenit Space Launch System from the Eyes of its Developers / Under the editorship of e.d. [...]

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

18.2.2017 Development Test of Payload Fairing Separation Dynamics under Ground Conditions

2017 (2); 102-106 Language: Russian Annotation: The paper presents the original test methods with simulation of axial loads nx＜＜ 1 and nx ＞＞1 and the test stands which were used on [...]

Read more 18.2.2017 Development Test of Payload Fairing Separation Dynamics under Ground Conditions

7.1.2017 Static Approach Application in Analysis of Gas-Dynamic Parameters in Launch Vehicle Vented Bays

By the example of Zenit LV it is shown that when using the statistic assessment, it is possible to considerably expand the launch vehicles application field from the [...]

Read more 7.1.2017 Static Approach Application in Analysis of Gas-Dynamic Parameters in Launch Vehicle Vented Bays