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15 search results for "tank"
9.1.2020 Experimental investigation of a liner-free propellant tank made from polymer composite materials
Experimental investigation of a liner-free propellant tank made from polymer composite materials Authors: Sidoruk А. 2020, (1); 90-98 DOI: [...]
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9.1.2018 On the Peculiarities of High-Temperature Rocket Propellants Drain from Delivery Means to Filling Tank for Closed Drain
On the Peculiarities of High-Temperature Rocket Propellants Drain from Delivery Means to Filling Tank for Closed Drain Authors: Pozdieiev H. 2018 (1); 53-57 DOI: [...]
Read more 9.1.2018 On the Peculiarities of High-Temperature Rocket Propellants Drain from Delivery Means to Filling Tank for Closed Drain
8.2.2017 Analysis Method of Nitrogen Tetroxide Tanks Generating Pressurization Systems
Analysis Method of Nitrogen Tetroxide Tanks Generating Pressurization Systems Authors: Petrenko R. 2017 (2); 41-48 Language: Russian Annotation: The paper considers the [...]
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7.1.2019 Experience of Development and Use of Generator Pressurization System for Tanks of Launch Vehicles on High-Temperature Propellants
Experience of Development and Use of Generator Pressurization System for Tanks of Launch Vehicles on High-Temperature Propellants Authors: Voloshin M. 2019, (1); 45-53 DOI: [...]
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5.2.2019 Features of the development testing of the propellants deposition inside the tanks of launch vehicles
Features of the development testing of the propellants deposition inside the tanks of launch vehicles Authors: Sedykh I. As the propellant during pauses between ignitions is [...]
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10.2.2017 Analysis Method of Hydraulic Parameters of Circular Intake Device in Limit Operating Modes
Experimental Investigation of Toroidal Tank Intake Device at High-Flowrate Flow Lab. On Measurement of Liquid Flow Discontinuity during Development Testing of Flying Vehicle [...]
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11.1.2020 Some results of strength calculations relying on analytical and FEM approaches. Trends of using contemporary machine learning strategies
An Investigation of a Spacecraft’s Propellant Tanks Shells Bearing Strength.
7.2.2017 Features of Pneumatic Hydraulic Feeding System with the Use of Oxygen-Methane Cryogenic Propellants
The optimal parameters are considered of pneumohydraulic supply system, including the designs of tanks, pressurization system and engine supply lines cooling system.
6.2.2017 Set of Actions on Enhancement of Launch Vehicle Payload Capability
2017 (2); 29-34 Language: Russian Annotation: The paper presents a complex of analytical calculation measures that allow increasing tanks useful volume and ensure engines’ [...]
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4.2.2017 Increase of LV Payload Capability through Enhancement of Propulsion System Pneudraulic System Characteristics
Rocket Propellant Tanks Pressurization Systems. Rocket Propellant Tank Pressurization Method / B. Evolution Tendencies of LV Propellant Tanks Pressurization [...]
Read more 4.2.2017 Increase of LV Payload Capability through Enhancement of Propulsion System Pneudraulic System Characteristics