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42 search results for "gas"
10.1.2020 Calculation and selection of parameters for a propellant consumption diagram of dual-thrust main SRM
Gasotermodinamika raketnykh dvigatelei na tverdom toplive.
19.2.2018 Control of Validity and Assessment of Accuracy of Telemetry Results during Full-Scale Test of Launch Vehicles
Use of Statistic Approaches in Analysis of Gas Dynamic Parameters in LV Vented Bays.
12.2.2018 Methodological Support for Initial Phase Optimization of Projecting Design, Trajectory Parameters and Rocket Object Motion Control Programs
Gas Dynamics of Powder Rocket Motors.
5.2.2018 Electromagnetic Valves Developed by Yuzhnoye SDO Liquid Rocket Engines Design Office
The present-day spacecraft gas-jet orientation and stabilization systems use as propulsion devices the electromagnetic valves with nozzles whose thrust is, as a rule, not [...]
Read more 5.2.2018 Electromagnetic Valves Developed by Yuzhnoye SDO Liquid Rocket Engines Design Office
4.2.2018 Turbopump Units of Rocket Engines Developed by DO-4
Having analyzed the data presented, one may conclude that the Rocket Engines Design Office and Yuzhnoye SDO as a whole accumulated sufficient experience and knowledge allowing [...]
Read more 4.2.2018 Turbopump Units of Rocket Engines Developed by DO-4
1.2.2018 Design Office of Liquid Rocket Engines is 60
Among them we should mention the RD858 and RD859 engines for the soviet lunar take-off-and –landing module of Block E, the unique RD857 and RD862 engines with afterburning of [...]
Read more 1.2.2018 Design Office of Liquid Rocket Engines is 60
13.1.2018 On Selection of Materials for Creation of Modern LV Thermostating System Mating Hoses
The Impact of Additives on Thermal Ageing of Rubbers and Model Gaskets Made of SKEP.
9.1.2018 On the Peculiarities of High-Temperature Rocket Propellants Drain from Delivery Means to Filling Tank for Closed Drain
2018 (1); 53-57 DOI: https://doi.org/10.33136/stma2018.01.053 Language: Russian Annotation: The paper presents the variation of parameters of gas-vapor mixture of hypergolic [...]
Read more 9.1.2018 On the Peculiarities of High-Temperature Rocket Propellants Drain from Delivery Means to Filling Tank for Closed Drain
8.1.2018 The Solid–Propellant Motors with Regulated Thrust
Solid Rocket Motor Gas Thermodynamics.
2.1.2018 Dehydration of Hydrocarbon Fuels by Method of Over-Saturation Drop
Calculated Evaluation and Experimental Check of RPC Degassing and Saturation by Helium for Filling Cyclone-4 LV: Technical Note Cyclone-4.