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, Petrenko Y. Content 2018 (1) Downloads: 35 Abstract views: 926 Dynamics of article downloads Dynamics of abstract views Downloads geography Country City Downloads USA Boardman; Ashburn; Ashburn; Baltimore; Boydton; Plano; Columbus; Detroit; Monroe; Ashburn; Seattle; Seattle; Ashburn; Seattle; San Mateo; San Mateo; San Mateo; Des Moines; Boardman; Boardman; Ashburn 21 Singapore Singapore; Singapore; Singapore; Singapore; Singapore; Singapore; Singapore 7 Philippines Cainta 1 Unknown 1 Türkiye Istanbul 1 Germany Falkenstein 1 Romania Voluntari 1 Netherlands Amsterdam 1 Ukraine Dnipro 1 Downloads, views for all articles Articles, downloads, views by all authors Articles for all companies Geography of downloads articles Noskov S. P., Petrenko Y. P., Petrenko Y. P., Petrenko Y. P., Petrenko Y. P., Petrenko Y. P., Petrenko Y.
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1. Modernization and Automation of Temperature Calculation of Measurement Errors of Climatic Chambers for Accelerated Environmental Tests

Authors:

Noskov S. I., Bondar’ М. А., Yeres L. O., Levchenko P. P., Petrenko Y. M.

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2018 (1); 3-5

DOI: https://doi.org/10.33136/stma2018.01.003

Language: Russian

Annotation: The description of the program and its work on the part of the user is given as well as a description of the software automation solution from the programmer’s side. The introduction of an automated program has significantly accelerated the process of attestation of climatic chambers.

Key words:

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1.1.2018 Modernization and Automation of Temperature Calculation of Measurement Errors of Climatic Chambers for Accelerated Environmental Tests
1.1.2018 Modernization and Automation of Temperature Calculation of Measurement Errors of Climatic Chambers for Accelerated Environmental Tests
1.1.2018 Modernization and Automation of Temperature Calculation of Measurement Errors of Climatic Chambers for Accelerated Environmental Tests
]]> 5.1.2017 Development of Working Liquid Discontinuity Measurement Procedure and Its Certification https://journal.yuzhnoye.com/content_2017_1/annot_5_1_2017-en/ Thu, 22 Jun 2023 12:48:29 +0000 https://journal.yuzhnoye.com/?page_id=29374
Development of Working Liquid Discontinuity Measurement Procedure and Its Certification Authors: Bondar’ М. , Petrenko Y. To ensure the uniformity of measurements when reducing this method to practice, the methodology of its certification experimental investigations is proposed for the purpose of determination of its applicability limits. М., Petrenko Y. (2017) "Development of Working Liquid Discontinuity Measurement Procedure and Its Certification" Космическая техника. "Development of Working Liquid Discontinuity Measurement Procedure and Its Certification" Космическая техника. М., Petrenko Y. quot;Development of Working Liquid Discontinuity Measurement Procedure and Its Certification", Космическая техника. М., Petrenko Y. М., Petrenko Y. М., Petrenko Y. М., Petrenko Y.
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5. Development of Working Liquid Discontinuity Measurement Procedure and Its Certification

Authors:

Bondar’ М. А., Huseva H. S., Yeres L. O., Kurako I. М., Petrenko Y. M., Rozmaita N. Yu.

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2017 (1); 30-34

Language: Russian

Annotation: The method not used before to measure discontinuity of working fluid using video recorders is considered. To ensure the uniformity of measurements when reducing this method to practice, the methodology of its certification experimental investigations is proposed for the purpose of determination of its applicability limits.

Key words:

Bibliography:

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5.1.2017 Development of Working Liquid Discontinuity Measurement Procedure and Its Certification
5.1.2017 Development of Working Liquid Discontinuity Measurement Procedure and Its Certification
5.1.2017 Development of Working Liquid Discontinuity Measurement Procedure and Its Certification
]]> 9.2.2016 Metrological Support of Kinematic Model Testing on Zero-Gravity Test Stands https://journal.yuzhnoye.com/content_2016_2-en/annot_9_2_2016-en/ Tue, 06 Jun 2023 11:56:39 +0000 https://journal.yuzhnoye.com/?page_id=28319
Metrological Support of Kinematic Model Testing on Zero-Gravity Test Stands Authors: Bondar’ М. , Petrenko Y. М., Petrenko Y. (2016) "Metrological Support of Kinematic Model Testing on Zero-Gravity Test Stands" Космическая техника. "Metrological Support of Kinematic Model Testing on Zero-Gravity Test Stands" Космическая техника. М., Petrenko Y. quot;Metrological Support of Kinematic Model Testing on Zero-Gravity Test Stands", Космическая техника. Metrological Support of Kinematic Model Testing on Zero-Gravity Test Stands Автори: Bondar’ М. М., Petrenko Y. Metrological Support of Kinematic Model Testing on Zero-Gravity Test Stands Автори: Bondar’ М. М., Petrenko Y. М., Petrenko Y. М., Petrenko Y.
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9. Metrological Support of Kinematic Model Testing on Zero-Gravity Test Stands

Authors:

Bondar’ М. А., Yeres L. O., Kurako I. М., Petrenko Y. M., Goltsev O. S.

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2016 (2); 60-64

Language: Russian

Annotation: Example of the estimate of the measurement error of the linear accelerations during the free fall of the kinematic model is considered. It was concluded that experiments on error measurements can be replaced with calculations for those parameters which have sufficient initial data on metrological performance of the applied instrumentation.

Key words:

Bibliography:

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9.2.2016 Metrological Support of Kinematic Model Testing on Zero-Gravity Test Stands
9.2.2016 Metrological Support of Kinematic Model Testing on Zero-Gravity Test Stands
9.2.2016 Metrological Support of Kinematic Model Testing on Zero-Gravity Test Stands
]]> 5.1.2019 Methodology of Normative Principles of Justification of Launch Vehicle Launching Facility Structures Lifetime https://journal.yuzhnoye.com/content_2019_1-en/annot_5_1_2019-en/ Thu, 25 May 2023 12:09:25 +0000 https://journal.yuzhnoye.com/?page_id=27710
Methodology of Normative Principles of Justification of Launch Vehicle Launching Facility Structures Lifetime Authors: Hudramovych V. Raschet na prochnost’ detaley machin: spravochnik. Stvorennya metodologii nornativnykh osnov rozrakhunku resursu konstruktsii startovykh sporud ksomichnykh raket-nosiiv / Teoria ta practika ratsionalnogo proektuvannya, vygotovlennya i ekspluatatsii machinobudivnykh konstruktsiy: materialy 6-oy Mizhnar. Petrenko. Osnovy otrabotky raketno -kosmicheskykh konstruktsiy: monografia. Hudramovych V. Methodology of Normative Principles of Justification of Launch Vehicle Launching Facility Structures Lifetime Автори: Hudramovych V.
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5. Methodology of Normative Principles of Justification of Launch Vehicle Launching Facility Structures Lifetime

Authors:

Hudramovych V. S.1, Sirenko V. M.2, Klimenko D. V.2, Daniyev Y. F.1, Hart Ye. L.3

Organization:

The Institute of Technical Mechanics, Dnipro, Ukraine1; Yangel Yuzhnoye State Design Office, Dnipro, Ukraine2; Oles Honchar Dnipro National University, Dnipro, Ukraine3

Page: Kosm. teh. Raket. vooruž. 2019, (1); 28-37

DOI: https://doi.org/10.33136/stma2019.01.028

Language: Russian

Annotation: This article contains results of methodology and standards development for life prediction of launch site structures to launch various types’ launch vehicles into near-earth orbit. Launch sites have been built in various countries of the world (European Union, India, China, Korea, Russia, USA, Ukraine, France, Japan, etc.). In different countries they have their own characteristics, depending on the type and performance of the launch vehicles, infrastructure features (geography of the site, nomenclature of the space objects, development level of rocket and space technology), problems that are solved during launches, etc. Solution of various issues, arising in the process of development of the standards for justification of launch site life is associated with the requirement to consider complex problems of strength and life of nonuniform structural elements of launch sites and structures of rocket and space technology. Launch sites are the combination of technologically and functionally interconnected mobile and fixed hardware, controls and facilities, designed to support and carry out all types of operations with integrated launch vehicles. Launch pad, consisting of the support frame, flue duct lining and embedded elements for frame mounting, is one of the principal components of the launcher and to a large extent defines the life of the launch site. Main achievements of Ukrainian scientists in the field of strength and life are specified, taking into account the specifics of various branches of technology. It is noted that the physical nonlinearity of the material and statistical approaches determine the strength analysis of useful life. Main methodological steps of launch site structures life prediction are defined. Service limit of launch site is suggested to be the critical time or the number of cycles (launches) over this period, after which the specified limiting states are achieved in the dangerous areas of the load-bearing elements: critical cracks, destruction, formation of unacceptable plastic deformations, buckling failure, corrosion propagation, etc. Classification of loads acting on the launch sites is given. The useful life of launch site is associated with estimation of the number of launches. Concept of low and multiple-cycle fatigue is used. Developing strength standards and useful life calculation basis, it is advisable to use modern methods of engineering diagnostics, in particular, holographic interferometry and acoustic emission, and to develop the high-speed circuits of numerical procedures for on-line calculations when testing the designed systems.

Key words: classification of loads and failures; shock wave, acoustic and thermal loads; low-cycle fatigue; hierarchical approach in classification; projection-iterative schemes of numerical procedur

Bibliography:

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5.1.2019 Methodology of Normative Principles of Justification of Launch Vehicle Launching Facility Structures Lifetime
5.1.2019 Methodology of Normative Principles of Justification of Launch Vehicle Launching Facility Structures Lifetime
5.1.2019 Methodology of Normative Principles of Justification of Launch Vehicle Launching Facility Structures Lifetime

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