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16 search results for "Dnepr LV"
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 [...]
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21.1.2020 Contemporary approaches to the improvement of methods of space launch system operation for commercial launches of ILV
Contemporary approaches to the improvement of methods of space launch system operation for commercial launches of ILV Authors: Hlechkov V. The article is of practical [...]
Read more 21.1.2020 Contemporary approaches to the improvement of methods of space launch system operation for commercial launches of ILV
15.1.2018 The Results of Using Automated Methods to Solve Standardization Tasks in Yuzhnoye SDO Practice
The Results of Using Automated Methods to Solve Standardization Tasks in Yuzhnoye SDO Practice Authors: Shipko O. 2018 (1); 91-100 DOI: [...]
Read more 15.1.2018 The Results of Using Automated Methods to Solve Standardization Tasks in Yuzhnoye SDO Practice
13.1.2018 On Selection of Materials for Creation of Modern LV Thermostating System Mating Hoses
On Selection of Materials for Creation of Modern LV Thermostating System Mating Hoses Authors: Bigun S. Investigation of Operability of Rubbers with Adhesion Additives in [...]
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14.2.2017 Development Test of Isolating Valve Operation under Cryogenic Conditions
Development Test of Isolating Valve Operation under Cryogenic Conditions Authors: Makarenko A. 2017 (2); 70-76 Language: Russian Annotation: The paper is about the ground [...]
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13.2.2017 Experience in Development of Isolating Fuel Valve with Pneumatic Drive and Hydraulic Brake for Operation under Cryogenic Conditions
Experience in Development of Isolating Fuel Valve with Pneumatic Drive and Hydraulic Brake for Operation under Cryogenic Conditions Authors: Makarenko A. 2017 (2); 65-69 [...]
Read more 13.2.2017 Experience in Development of Isolating Fuel Valve with Pneumatic Drive and Hydraulic Brake for Operation under Cryogenic Conditions
4.2.2017 Increase of LV Payload Capability through Enhancement of Propulsion System Pneudraulic System Characteristics
Increase of LV Payload Capability through Enhancement of Propulsion System Pneudraulic System Characteristics Authors: Logvinenko A. Evolution Tendencies of LV [...]
Read more 4.2.2017 Increase of LV Payload Capability through Enhancement of Propulsion System Pneudraulic System Characteristics
18.1.2019 Designing of Servo Driver of Throttle Mechanisms and Fuel Flow Regulator of ILV Main Motor
Designing of Servo Driver of Throttle Mechanisms and Fuel Flow Regulator of ILV Main Motor Authors: Oslavsky S. 2019, (1); 122-131 DOI: [...]
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2.1.2020 Analysis of development trends of design parameters and basic characteristics of missiles for the advanced multiple launch rocket systems
Dnepropetrovsk, 2014. I., Lvov А. Dnepropetrovsk, 2017.
5.1.2024 Assessment of risk of toxic damage to people in case of a launch vehicle accident at flight
2024, (1); 40-50 DOI: https://doi.org/10.33136/stma2024.01.040 Language: English Annotation: Despite stringent environmental requirements, modern launch vehicles/integrated launch [...]
Read more 5.1.2024 Assessment of risk of toxic damage to people in case of a launch vehicle accident at flight