19.1.2020 Pyrobolts: types, design, development. Shear type pyrobolt developed at Yuzhnoye SDO

Pyrobolts: types, design, development. Owing to the simple design, reliability and short action time, the pyrobolts have found wide application in aerospace [...]

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18.1.2020 Development of autonomous power engineering systems with hydrogen energy storage

Development of autonomous power engineering systems with hydrogen energy storage Authors: Shevchenko A. (2020) "Development of autonomous power [...]

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8.2.2018 Development of Nozzle Blocks New Manufacturing Technology without Blazing

Development of Nozzle Blocks New Manufacturing Technology without Blazing Authors: Kovalenko A. The step-by-step sequence and procedure of research work to develop and [...]

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4.2.2018 Turbopump Units of Rocket Engines Developed by DO-4

Both earlier developments of DO and the turbopump unit being now in final testing phase are considered. Having analyzed the data presented, one may conclude that the [...]

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3.2.2018 Possible Ways of Modernization of VEGA Launch Vehicle AVUM Stage Main Engine Assembly

This LRE has a combination of attractive characteristics, such as high specific pulse, low mass, multiple ignitions in flight, high reliability confirmed by good results of flight [...]

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2.2.2018 Yuzhnoye SDO-Developed Upper Stage Liquid Rocket Engines

Key words: main engine , engine development test , takeoff-and-landing module , pneumatic pump unit Bibliography: 1. main engine , engine [...]

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1.2.2018 Design Office of Liquid Rocket Engines is 60

2018 (2); 3-7 DOI: https://doi.org/10.33136/stma2018.02.003 Language: Russian Annotation: During 60 years of existence of specialized Liquid Rocket Engines Design Office – [...]

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20.2.2017 Research Support for Development of Launch Vehicle Payload Unit Composite Load-Bearing Compartments

Development of Methods to Design Space Rocketry Composite Materials and Structures: Dissertation of Doctor of Engineering Science: 05.07.02, 05.02.01. Static [...]

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17.2.2017 Development Test of Spacecraft Separation Dynamics under Ground Conditions

Development Test of Spacecraft Separation Dynamics under Ground Conditions Authors: Gontarovsky V. Theory of Engineering Experiment. (2017) [...]

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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

2017 (2); 65-69 Language: Russian Annotation: To support ignition of Taurus LV first stage core structure engine, an oxidizer dividing valve has been developed that ensures [...]

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