Search Results for “Fomenko V. S.” – Collected book of scientific-technical articles https://journal.yuzhnoye.com Space technology. Missile armaments Tue, 02 Apr 2024 08:11:17 +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 “Fomenko V. S.” – Collected book of scientific-technical articles https://journal.yuzhnoye.com 32 32 8.1.2018 The Solid–Propellant Motors with Regulated Thrust https://journal.yuzhnoye.com/content_2018_1-en/annot_8_1_2018-en/ Tue, 05 Sep 2023 06:26:08 +0000 https://journal.yuzhnoye.com/?page_id=30458
The Solid–Propellant Motors with Regulated Thrust Authors: Glazkov V. , Fomenko V. I., Sokoovsky M. Presnyakov V. Content 2018 (1) Downloads: 13 Abstract views: 374 Dynamics of article downloads Dynamics of abstract views Downloads geography Country City Downloads USA Boardman; Plano; Monroe; Seattle; Ashburn; San Mateo; Boardman; Ashburn 8 Singapore Singapore; Singapore; Singapore; Singapore 4 Ukraine Dnipro 1 Downloads, views for all articles Articles, downloads, views by all authors Articles for all companies Geography of downloads articles Glazkov V. R., Fomenko V. R., Fomenko V. Missile armaments, vol. The Solid–Propellant Motors with Regulated Thrust Автори: Glazkov V. R., Fomenko V. R., Fomenko V. R., Fomenko V. R., Fomenko V.
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8. The Solid–Propellant Motors with Regulated Thrust

Authors:

Glazkov V. O., Yenotov V. H., Kozak L. R., Fomenko V. S.

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2018 (1); 46-52

DOI: https://doi.org/10.33136/stma2018.01.046

Language: Russian

Annotation: The paper considers the results of scientific research and experimental works performed by Yuzhnoye SDO on solid–propellant motors with controlled thrust. The possibility in principle is shown of creating such motors and stabilizing their characteristics in different operation modes due to the throat area regulation system and selection of relevant control algorithm.

Key words:

Bibliography:
1. Petrenko V. I., Sokoovsky M. I. et al. Control of Solid-Propellant Propulsion Systems. М., 2003. 463 p.
2. Presnyakov V. F. Solid Rocket Motor Dynamics. М., 1984. 248 p.
3. Sorokin R. E. Solid Rocket Motor Gas Thermodynamics. М., 1967. 368 p.

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8.1.2018 The Solid–Propellant Motors with Regulated Thrust
8.1.2018 The Solid–Propellant Motors with Regulated Thrust
8.1.2018 The Solid–Propellant Motors with Regulated Thrust
]]> 11.1.2017 Environmental Safety of Bench Testing the Advanced Solid-Propellant Rocket Motors https://journal.yuzhnoye.com/content_2017_1/annot_11_1_2017-en/ Wed, 28 Jun 2023 12:21:35 +0000 https://journal.yuzhnoye.com/?page_id=29442
Environmental Safety of Bench Testing the Advanced Solid-Propellant Rocket Motors Authors: Sokolov O. , Fomenko V. Gusev N. V., Sheiko А. F., Fomenko V. V., Sheiko А. F., Fomenko V. Missile armaments, vol. Environmental Safety of Bench Testing the Advanced Solid-Propellant Rocket Motors Автори: Sokolov O. V., Sheiko А. F., Fomenko V. Environmental Safety of Bench Testing the Advanced Solid-Propellant Rocket Motors Автори: Sokolov O. V., Sheiko А. F., Fomenko V. Environmental Safety of Bench Testing the Advanced Solid-Propellant Rocket Motors Автори: Sokolov O. V., Sheiko А. F., Fomenko V. Environmental Safety of Bench Testing the Advanced Solid-Propellant Rocket Motors Автори: Sokolov O. V., Sheiko А. F., Fomenko V.
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11. Environmental Safety of Bench Testing the Advanced Solid-Propellant Rocket Motors

Authors:

Sokolov O. V., Sheiko А. F., Fomenko V. S., Kirichenko A. S.

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2017 (1); 70-77

Language: Russian

Annotation: The mathematical models are presented and the calculations are made of lower atmosphere contamination with solid propellant combustion products, noise and thermal effects on environment in the test bench area. Based on earlier field investigations and on the results obtained, the assessment is given of ecological safety of the tests.

Key words:

Bibliography:
1. Noise Control in Industry: Guide / Under the editorship of E. Y. Yudin. М., 1985.
2. Maximum Permissible Concentrations and Approximate Safe Levels of Contaminating Substances Effect in Atmospheric Air of Populated Areas. Donetsk, 2000.
3. GOST 12.1.005-88. System of Labor Safety Standards. General Sanitary-Hygienic Requirements to Working Area Air / Collection of GOSTs. М., 1988.
4. Gusev N. G., Belyayev V. A. Radioactive Emissions in Biosphere: Guide. 2nd edition. M., 1991. 256 p.
5. Investigation of Environment Pollution during Tests of 365-Type Article on PMZ Site: Report on research work / MPO Technokhim, NPO GIPH. Leningrad, 1991.
6. Assessment of Hygienic Situation in the Area of Pavlograd Mechanical Plant during Tests of 15D365 Articles. Report by Agreement No48-6/91-429 YuR-1/Ministry of Health Protection of the USSR. M., 1991.

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11.1.2017 Environmental Safety of Bench Testing the Advanced Solid-Propellant Rocket Motors
11.1.2017 Environmental Safety of Bench Testing the Advanced Solid-Propellant Rocket Motors
11.1.2017 Environmental Safety of Bench Testing the Advanced Solid-Propellant Rocket Motors
]]> 9.1.2016 Evaluation of SRM Intraballistic Parameters Scatter by Monte-Carlo Method https://journal.yuzhnoye.com/content_2016_1/annot_9_1_2016-en/ Tue, 23 May 2023 13:04:25 +0000 https://journal.yuzhnoye.com/?page_id=27617
Evaluation of SRM Intraballistic Parameters Scatter by Monte-Carlo Method Authors: Fomenko V. Content 2016 (1) Downloads: 21 Abstract views: 122 Dynamics of article downloads Dynamics of abstract views Downloads geography Country City Downloads USA Boardman; Baltimore; Plano; Monroe; Seattle; Ashburn; Boardman; Seattle; Seattle; San Mateo; Boardman; Ashburn 12 Singapore Singapore; Singapore; Singapore; Singapore; Singapore; Singapore; Singapore 7 Ukraine Dnipro; Dnipro 2 Downloads, views for all articles Articles, downloads, views by all authors Articles for all companies Geography of downloads articles Fomenko V. Evaluation of SRM Intraballistic Parameters Scatter by Monte-Carlo Method Автори: Fomenko V. Evaluation of SRM Intraballistic Parameters Scatter by Monte-Carlo Method Автори: Fomenko V. Evaluation of SRM Intraballistic Parameters Scatter by Monte-Carlo Method Автори: Fomenko V. Evaluation of SRM Intraballistic Parameters Scatter by Monte-Carlo Method Автори: Fomenko V.
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9. Evaluation of SRM Intraballistic Parameters Scatter by Monte-Carlo Method

Authors:

Fomenko V. S., Kalnysh R. V., Popov V. A.

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2016 (1); 59-62

Language: Russian

Annotation: The purpose of work is development of simple and accurate procedure of calculation of scatter of SRM intraballistic parameters – combustion chamber pressure and combustion products flow rate. The problem is solved by Monte Carlo method (statistic tests) which allows constructing the function of distribution of composition (sum, product) of random values of specified distribution laws. The accuracy of problem solution is determined by quality of pseudo random values generation.

Key words:

Bibliography:

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9.1.2016 Evaluation of SRM Intraballistic Parameters Scatter by Monte-Carlo Method
9.1.2016 Evaluation of SRM Intraballistic Parameters Scatter by Monte-Carlo Method
9.1.2016 Evaluation of SRM Intraballistic Parameters Scatter by Monte-Carlo Method
]]> 8.1.2016 Assessment of Validity of Hypothesis of Constancy of Specific Vacuum Thrust Pulse during SRM Designing and Testing https://journal.yuzhnoye.com/content_2016_1/annot_8_1_2016-en/ Tue, 23 May 2023 13:03:08 +0000 https://journal.yuzhnoye.com/?page_id=27614
S., Fomenko V. S., Fomenko V. S., Fomenko V. S., Fomenko V. S., Fomenko V. S., Fomenko V.
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8. Assessment of Validity of Hypothesis of Constancy of Specific Vacuum Thrust Pulse during SRM Designing and Testing

Authors:

Kalnysh R. V., Kirichenko A. S., Fomenko V. S.

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2016 (1); 55-58

Language: Russian

Annotation: In the phase of designing and developmental testing of short-range missiles with main solid rocket motors, the necessity arises of quick evaluation of propulsion system power characteristics, in particular, determination of specific thrust pulse value and scatter. The use of hypothesis of specific thrust constancy (weak dependence of vacuum thrust pulse on pressure and temperature) allows to considerably simplify the procedure of SRM specific thrust pulse evaluation, thus increasing the efficiency of SRM design calculations and the speed of test results processing, and in some cases, even to considerably reduce the test scope.

Key words:

Bibliography:

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8.1.2016 Assessment of Validity of Hypothesis of Constancy of Specific Vacuum Thrust Pulse during SRM Designing and Testing
8.1.2016 Assessment of Validity of Hypothesis of Constancy of Specific Vacuum Thrust Pulse during SRM Designing and Testing
8.1.2016 Assessment of Validity of Hypothesis of Constancy of Specific Vacuum Thrust Pulse during SRM Designing and Testing
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