7.2.2017 Features of Pneumatic Hydraulic Feeding System with the Use of Oxygen-Methane Cryogenic Propellants

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6.2.2017 Set of Actions on Enhancement of Launch Vehicle Payload Capability

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5.2.2017 Structural Perfection of Cyclone-4 Integrated Launch Vehicle

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4.2.2017 Increase of LV Payload Capability through Enhancement of Propulsion System Pneudraulic System Characteristics

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1.2.2017 DO-2 – Semicentenary

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3.2.2017 Creation of Advanced Facilities for Spacecraft / Launch Vehicle Integration

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File of Issue № 1 (2017)

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File of Issue № 2 (2019)

2019, (2); 103-108 https://doi.org/10.33136/stma2019.02.103 Annotation | Full Text (PDF) на сайт ДП «КБ «Південне» Visits:2781

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1.1.2017 Methodology for Measurement Uncertainty Evaluation during Metrological Certification of Measuring Instruments

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10.1.2017 Features of Measurement System for Gas-Dynamic Model Tests of Rocket Complex Elements

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