Investigating the thermohydraulic efficiency of the liquid-propellant rocket engine porous tract of cooling with the interchannel coolant flow
| Authors: Anfimov M.V. | Published: 17.10.2017 |
| Published in issue: #10(15)/2017 | |
| DOI: DOI: 10.18698/2541-8009-2017-10-188 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: Thermohydraulic efficiency, porous tract, liquid-propellant rocket engine cooling, thermal protection | |
Usage of oxygen-and-methane propellant in liquid-propellant rocket engines
| Authors: Bregvadze D.T., Gabidulin O.V., Gurkin A.A., Zabolotko I.A. | Published: 29.11.2017 |
| Published in issue: #12(17)/2017 | |
| DOI: DOI: 10.18698/2541-8009-2017-12-205 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: liquid-propellant rocket engines, liquid methane, prospective rocket fuel, cooling of rocket engine, fuel-to-oxidizer ratio | |
Comparative analysis of the operation of liquid-fuel rocket engine pump turbine if equipped with the auxiliary booster pump package
| Authors: Ivashin V.S., Anishchenko Yu.V. | Published: 20.12.2017 |
| Published in issue: #1(18)/2018 | |
| DOI: DOI: 10.18698/2541-8009-2018-1-225 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
| Keywords: pump turbine, booster pump package, fuel feed system, spin rate, pump speed coefficient, rocket engine | |
Implementation of the universal asynchronous receiver-transmitter on the programmable logical integrated circuit die
| Authors: Ronzhin I.V., Makarova A.V. | Published: 12.04.2018 |
| Published in issue: #4(21)/2018 | |
| DOI: DOI: 10.18698/2541-8009-2018-4-295 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
| Keywords: programmable logical integrated circuits, universal asynchronous receiver-transmitter, UART data protocol, RX receiver circuit, TX transmitter circuit, implementation of UART in programmable logical integrated circuits | |
Application of multipropellant fuel in rocket engines
| Authors: Kalugin K.S. | Published: 27.04.2018 |
| Published in issue: #5(22)/2018 | |
| DOI: DOI: 10.18698/2541-8009-2018-5-304 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: rocket fuel, multipropellant fuel, pseudoliquified powdered metalized fuel, aerojet engine, hydro jet engine, chemical fuel, liquid rocket engine | |
Selecting the loop gains of the unmanned aerial vehicle pitch attitude control system with allowance for tolerances on the aerodynamic and mass centering characteristics
| Authors: Fam Suan Chyong | Published: 28.05.2018 |
| Published in issue: #5(22)/2018 | |
| DOI: DOI: 10.18698/2541-8009-2018-5-317 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: unmanned aerial vehicle, flight control system, attitude control system, stabilization law, cruise missile, Kharitonov theorem, D-partitioning method, robust stability | |
Localization of the object by means of its acoustic signal
| Authors: Troshina E.Yu. | Published: 18.06.2018 |
| Published in issue: #6(23)/2018 | |
| DOI: DOI: 10.18698/2541-8009-2018-6-331 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: acoustic direction finder, correction function, identifying the position, mathematical model, sound source, miniature microphones, broadband signal, signal delay | |
Analytic investigation of the approaches to increasing the navigational accuracy of the pulse-corrected aircraft
| Authors: Vedenichev I.V. | Published: 24.07.2018 |
| Published in issue: #7(24)/2018 | |
| DOI: DOI: 10.18698/2541-8009-2018-7-341 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: ballistic analysis, pulse correction, accuracy increase, corrected missile, low trajectory, high trajectory, MATLAB, Simulink, flight simulation | |
Development of the method of ultrastrial diagnostics of a cutting tool for utilization of polymer composite materials in the design of rocket-space technology
| Authors: Li Syueyan, Semashko V.V., Abashin M.I. | Published: 27.08.2018 |
| Published in issue: #8(25)/2018 | |
| DOI: DOI: 10.18698/2541-8009-2018-8-363 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Innovation Technologies of Aerospace Engineering | |
| Keywords: recycling, polymer composite material, ultra-jet diagnostics, imitation, wear, cutting edge, hydro-jet, rocket technology | |