| Issue |
Section |
Title |
File |
| Vol 12, No 2 (2013) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Investigation of energy parameters of small-thrust liquid rocket engines with the geometric expansion ratio of the nozzle F=200 |
(Rus)
|
| Vol 8, No 3-2 (2009): Special Issue |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Mathematical modelling and parametric research of flow of the twisted turbulent single-component stream of the propulsive mass in the trance- and supersonic areas of Laval nozzles |
(Rus)
|
| Vol 8, No 3-3 (2009): Special Issue |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Oxyhydrogen propulsion device base on water electrolysis and lrest on component H2 + O2 for control system SS |
(Rus)
|
| Vol 11, No 3-3 (2012): Special Issue |
CONFERENCE MATERIALS |
Research of influence of the thermal stream from the mid-flight liquid rocket engine on parameters of operating liquid rocket engines of small draught in the conditions of perspective razgonnogo's propulsion system of the block |
(Rus)
|
| Vol 13, No 5-2 (2014): Special Issue |
ISSUE WITHOUT SECTION |
Automated thermovacuum firing test facility for testing and research of workflow in low-thrust rocket engine on hypergolic propellants |
(Rus)
|
| Vol 13, No 5-3 (2014): Special Issue |
ISSUE WITHOUT SECTION |
Results of experimental studies of parameters of low-thrust rocket engines operating on gaseous oxygen-hydrogen fuel |
(Rus)
|
| Vol 15, No 4 (2016) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Efficiency of aft diffusers in vacuum systems of test benches for high-altitude firing tests of low-thrust liquid rocket engines |
(Rus)
|
| Vol 16, No 2 (2017) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Multi-purpose high-precision thermal vacuum testing bench and someresults of firing tests of non-hypergolic low-thrust rocket engines |
(Rus)
|
| Vol 17, No 3 (2018) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Choosing the mixing pattern for oxygen-hydrogen low-thrust rocket engines |
(Rus)
|
| Vol 17, No 4 (2018) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Propulsion systems and low-thrust rocket engines based on various physical principles for control systems of small and micro-spacecraft |
(Rus)
|
| Vol 18, No 2 (2019) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Technology of computational analysis of the working process parameters of low-thrust rocket engines running on gaseous oxygen-hydrogen fuel with the use of ANSYS CFD |
(Rus)
|
| Vol 10, No 3-3 (2011): Special Issue |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Research of the possibility of thermal conditions LREST using an infrared thermal imaging system |
(Rus)
|
| Vol 18, No 3 (2019) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Сalculated analysis of the influence of operation and design factors on the parameters of oxygen-hydrogen low-thrust rocket engines |
(Rus)
|
| Vol 18, No 4 (2019) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Computer-aided design of low-thust rocket engines using the domain-specific knowledge database and CAE / CAD systems |
(Rus)
|
| Vol 20, No 4 (2021) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
The structure of knowledge base to support the development of low-thrust liquid-propellant rocket engines based on computer technologies |
(Rus)
|
