Search Results for “Yelansky Y. A.” – Collected book of scientific-technical articles https://journal.yuzhnoye.com Space technology. Missile armaments Tue, 02 Apr 2024 07:24:45 +0000 en-GB hourly 1 https://wordpress.org/?v=6.2.2 https://journal.yuzhnoye.com/wp-content/uploads/2020/11/logo_1.svg Search Results for “Yelansky Y. A.” – Collected book of scientific-technical articles https://journal.yuzhnoye.com 32 32 12.1.2017 Static Performance Prediction of Hot-Gas Flapper-Nozzle Actuator https://journal.yuzhnoye.com/content_2017_1/annot_12_1_2017-en/ Fri, 22 Sep 2023 15:14:35 +0000 https://journal.yuzhnoye.com/?page_id=31702
Yelansky, V.
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12. Static Performance Prediction of Hot-Gas Flapper-Nozzle Actuator

Authors:

Tsyganov V. M.

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2017 (1); 78-83

Language: Russian

Annotation: The basic mathematical relations are considered to construct static characteristics of nozzle-shutter twostage piston pneumatic drive with the working medium – powder combustion products.

Key words:

Bibliography:
1. Oleinik V. P. et al. Static Characteristics of Gas Drive with Jet Engine / V. P. Oleinik, Y. A. Yelansky, V. N. Kovalenko, L. G. Kaluger, Е. V. Vnukov. Space Technology. Missile Armaments: Collection of scientific-technical articles. 2015. Issue. 1. P. 21-27.
2. Kornilov Y. G. et al. Pneumatic Elements and Systems. К., 1968. 143 p.
3. Hydraulic and Pneumatic Power Control System / Under the editorship of J. Blackborn, H. Reethoff, G. L. Sherer. М., 1962. 614 p.
4. Mertaf S. A. Tutorial on the Theory of Electrohydraulic Servo Mechanism with Acceleration Control Operating in Switchover Mode. Problems of Rocket Engineering. 1961. No. 2. P. 74-95.
5. Banshtyk A. М. Electrohydraulic Servo Mechanisms with Pulse-Width Control. М., 1972. 144 p.

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12.1.2017 Static Performance Prediction of Hot-Gas Flapper-Nozzle Actuator
12.1.2017 Static Performance Prediction of Hot-Gas Flapper-Nozzle Actuator
12.1.2017 Static Performance Prediction of Hot-Gas Flapper-Nozzle Actuator
]]> 9.1.2017 Mathematical Simulation of Gas-Jet Control System Distributor for Launch Vehicles https://journal.yuzhnoye.com/content_2017_1/annot_9_1_2017-en/ Tue, 27 Jun 2023 12:09:02 +0000 https://journal.yuzhnoye.com/?page_id=29434
, Yelansky Y. P., Yelansky Y. P., Yelansky Y. P., Yelansky Y. P., Yelansky Y. P., Yelansky Y. P., Yelansky Y.
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9. Mathematical Simulation of Gas-Jet Control System Distributor for Launch Vehicles

Authors:

Oliinyk V. P., Yelansky Y. A., Kaluger L. G.

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2017 (1); 59-66

Language: Russian

Annotation: The differential equations of the gas-jet control system two-stage hot gas distributor are considered.

Key words:

Bibliography:
1. Belyayev N. M., Uvarov E. I. Calculation and Designing of Spacecraft Reaction Control Systems. М., 1974. 200 p.
2. Volkov E. B., Golovkov L. T., Syritsin Т. А. Liquid Rocket Engines. М., 1970. 592 p.
3. Abramovich G. N. Applied Gas Dynamics. М., 1976. 888 p.
4. Mamontov M. A. Some Cases of Gas Flowing in Pipes, Heads and Flow Vessels. М., 1951. 469 p.
5. Gerz E. V., Kreinin G. V. Dynamics of Pneumatic Actuators of Automatic Machines. М., 1964. 233 p.
6. Flying Vehicle Control System Pneumatic Actuators / V. A. Chashhin, О. Т. Kamladze, А. B. Kondrat’yev et al. М., 1987. 248 p.
7. Simakov N. N. Experimental Confirmation of Early Critical Region on Single Sphere. Journal of Technical Physics. Vol. 80, Issue 7. 2010.
8. Deich М. Е. Technical Gas Dynamics. М.-L., 1961. 412 p.
9. Sitnikov B. T., Matveyev I. B. Calculation and Investigation of Safety and Relief Valves. М., 1972. 127 p.
10. Danilov Y. A., Kirillovsky Y. L., Kolpakov Y. G. Equipment of Massive Hydraulic Actuators: Operating Processes and Characteristics. М., 1990. 272 p.

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9.1.2017 Mathematical Simulation of Gas-Jet Control System Distributor for Launch Vehicles
9.1.2017 Mathematical Simulation of Gas-Jet Control System Distributor for Launch Vehicles
9.1.2017 Mathematical Simulation of Gas-Jet Control System Distributor for Launch Vehicles
]]> 12.2.2016 The Use of Thermoelectric Technologies in Spacecraft Thermostatic Systems https://journal.yuzhnoye.com/content_2016_2-en/annot_12_2_2016-en/ Tue, 06 Jun 2023 12:00:29 +0000 https://journal.yuzhnoye.com/?page_id=28325
, Yelansky Y. V., Yelansky Y. V., Yelansky Y. V., Yelansky Y. V., Yelansky Y. V., Yelansky Y. V., Yelansky Y.
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12. The Use of Thermoelectric Technologies in Spacecraft Thermostatic Systems

Authors:

Loza O. V., Yelansky Y. A., Pokatayev V. M., Karzova O. O.

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2016 (2); 75-79

Language: Russian

Annotation: Considered is the application of the thermoelectric cooling modules to enhance the operating reliability of the spacecraft’s temperature control system in the severe climatic conditions, schematic diagram of the thermoelectric cooling system is given.

Key words:

Bibliography:

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12.2.2016 The Use of Thermoelectric Technologies in Spacecraft Thermostatic Systems
12.2.2016 The Use of Thermoelectric Technologies in Spacecraft Thermostatic Systems
12.2.2016 The Use of Thermoelectric Technologies in Spacecraft Thermostatic Systems
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