| 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 5, No 2-2 (2006): Special Issue |
TECHNICAL SCIENCES |
Interaction of drops of a plume of a liquid with heated granulouse units |
(Rus)
|
| Vol 5, No 2-2 (2006): Special Issue |
TECHNICAL SCIENCES |
The concept and the results of elaboration of the automated test bench for testing the rocket engine |
(Rus)
|
| Vol 8, No 3-2 (2009): Special Issue |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Features of calculation of hydraulic characteristics of capillary spray jets of is liquid-stnyh rocket engines of small pull-rod |
(Rus)
|
| Vol 8, No 3-2 (2009): Special Issue |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
The flowing reactor as the tool of an experimental research of processes of transformation self-igniting liquid rocket fuel |
(Rus)
|
| Vol 8, No 3-2 (2009): Special Issue |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Research of laws of interaction of components in a liquid phase self-igniting liquid rocket fuel |
(Rus)
|
| Vol 11, No 3-3 (2012): Special Issue |
CONFERENCE MATERIALS |
Ways to improve the workflow of liquid rocket thrusters on hypergolic propellants |
(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 5-2 (2014): Special Issue |
ISSUE WITHOUT SECTION |
Investigation of transformation of intermediate products of liquid-phase interaction propellant at the onset of combustion for rocket engine |
(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 15, No 4 (2016) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Peculiarities of the working process of low-thrust hypergolic-propellant liquid rocket engines with a thrust of less than 1 N |
(Rus)
|
| Vol 10, No 3-3 (2011): Special Issue |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Investigation of the kinetic properties of gas products of liquid-phase interaction hypergolic liquid rocket fuel |
(Rus)
|
| Vol 10, No 3-3 (2011): Special Issue |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Increasing the energy efficiency of liquid rocket engine of small thrust (0,1-1,0) N with jet scheme of mixing |
(Rus)
|
| Vol 10, No 3-3 (2011): Special Issue |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Influence in a constructive and regime parameters antechamber by operation-in the combustion chamber liquid-propellant rocket engine thrusters on hypergolic liquid propellants |
(Rus)
|
