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22 search results for "fuel"
9.1.2020 Experimental investigation of a liner-free propellant tank made from polymer composite materials
Composite fuel tank for ILV, Dnipro, Yuzhnoye SDO, 2019.
17.2.2018 Peculiarities of Dynamics of Recoverable Part of Stage of Aircraft-Type Configuration with Turbojet Engine
This recovery plan differs from an alternative rocket recovery system and, from our point of view, provides more efficient usage of the fuel stores because it doesn’t require [...]
Read more 17.2.2018 Peculiarities of Dynamics of Recoverable Part of Stage of Aircraft-Type Configuration with Turbojet Engine
16.2.2018 Design Solutions to Prevent Propellant Ingress into SRM Case Space behind Sealing Ring
2018 (2); 139-142 DOI: https://doi.org/10.33136/stma2018.02.139 Language: Russian Annotation: The structure examined herein aims to keep fuel from entering the space behind [...]
Read more 16.2.2018 Design Solutions to Prevent Propellant Ingress into SRM Case Space behind Sealing Ring
9.2.2018 The Impact of Worm Design on Power and Anti-Cavitation Properties of Worm-Centrifugal Pumps
RD868 engine oxidizer and fuel pumps; RD859 engine fuel pumps; RD861K engine fuel pumps.
8.2.2017 Analysis Method of Nitrogen Tetroxide Tanks Generating Pressurization Systems
Calculation of Long-Range Missiles Fuel (UDMH) Tanks Pressurization with Hot Gases.
15.1.2017 Assessment of Liquid Equipment Neutralization Method Effectiveness
Rockets and Spacecraft Fueling Complex.
7.1.2019 Experience of Development and Use of Generator Pressurization System for Tanks of Launch Vehicles on High-Temperature Propellants
2019, (1); 45-53 DOI: https://doi.org/10.33136/stma2019.01.045 Language: Russian Annotation: Long-term experience in development, development testing and use of generating systems [...]
Read more 7.1.2019 Experience of Development and Use of Generator Pressurization System for Tanks of Launch Vehicles on High-Temperature Propellants
6.1.2019 Investigation into Peculiarities of Delivery to Launch Base of Rocket Propellant with Specified Gasing
In order to solve this problem number of factors have been considered, which determine the value of gas saturation in the propellants delivered to the launch site and procedure to [...]
Read more 6.1.2019 Investigation into Peculiarities of Delivery to Launch Base of Rocket Propellant with Specified Gasing
14.1.2019 Technique of Determination of SRM Operational Life Taking into Account Materials and Elements Strength Margins
Analysis of experimental and computation data as applied to solid-propellant rocket engine shows that the most dangerous zones, which define the service life, are the fuel [...]
Read more 14.1.2019 Technique of Determination of SRM Operational Life Taking into Account Materials and Elements Strength Margins
13.1.2019 Prediction of Solid Propellant Burnout Time in Launch Vehicle Propulsion System in Flight
2019, (1); 87-94 DOI: https://doi.org/10.33136/stma2019.01.088 Language: Russian Annotation: This article considers the problem of determination of propulsion system solid [...]
Read more 13.1.2019 Prediction of Solid Propellant Burnout Time in Launch Vehicle Propulsion System in Flight