Computational and experimental study of the characteristics of an exhaust diffuser with a central body as part of an altitude test facility for ground development testing of liquid rocket engines

More works in this specialty

1. Working processes in a low-thrust rocket engine operating on the gaseous propellant components oxygen and methane

   Chudina, Yuliya Sergeyevna · 2014 · Candidate of Sciences · Moscow State Aviation Institute

   • 05.07.05 Thermal, electric-rocket engines and power plants of aircraft
2. Mathematical modeling and numerical analysis of working processes in micro liquid-propellant rocket engines based on MEMS technologies

   Yakutin, Aleksandr Vladimirovich · 2010 · Candidate of Sciences · Moscow State Aviation Institute

   • 05.07.05 Thermal, electric-rocket engines and power plants of aircraft
3. Optimization of the design development process for low-thrust liquid-propellant rocket engines during hot-fire tests

   Yatsunenko, Vladimir Grigoryevich · 2006 · Candidate of Sciences

   • 05.07.05 Thermal, electric-rocket engines and power plants of aircraft
4. Selection of energy-mass characteristics of reusable sustainer liquid-propellant rocket engines using liquefied natural gas

   Klepikov, Igor Alekseevich · 2005 · Doctor of Sciences · Bauman Moscow State Technical University

   • 05.07.05 Thermal, electric-rocket engines and power plants of aircraft
5. Numerical and experimental investigation of the flow in the nozzle of a two-phase gas-droplet flow with a high mass concentration of liquid in the gas

   Yakovlev, Aleksey Aleksandrovich · 2004 · Candidate of Sciences

   • 05.07.05 Thermal, electric-rocket engines and power plants of aircraft

All works in this specialty