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1 , Titarenko V. 1 ORCID , Titarenko V. O., Titarenko V. O., Titarenko V. O., Titarenko V. O., Titarenko V. O., Titarenko V. O., Titarenko V. O., Titarenko V. O., Titarenko V. O., Titarenko V. O., Titarenko V. O., Titarenko V. O., Titarenko V. O., Titarenko V. O., Titarenko V.
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2. Predicting pulsed current parameters to produce nickel coatings with fine-grained textures

Date of receipt of the article for publication: 06.08.2026

Date of acceptance of the article for publication after review: 18.09.2026

Date of publication: 02.11.2026

ISSN: 2617-5525

e-ISSN: 2617-5533

ORCID authors:

Zabludovskyi V. O.1 ORCID, Titarenko V. V.2 ORCID

Organization:

Page: Kosm. teh. Raket. vooruž. 2026, (1); 14-22

Language: Ukrainian

Annotation: The paper investigates how the parameters of a pulsed unipolar current infl uence the process of applying nickel coatings by electrodeposition, as well as their structure, substructure, mechanical properties, and protective features, with a view to developing coatings for highly loaded components of rocket and space technologies. Based on comprehensive electrochemical and mechanical studies involving metallography and X-ray diff raction, the optimum parameters of a pulsed electrodeposition process have been determined to produce nickel coatings with fi ne-grained textures that feature high microhardness, adhesion strength, and corrosion resistance. The paper shows that, compared to coating deposition using direct current, the application of pulsed current promotes the formation of a more even and smoother surface that is free from typical defects. It has been found that non-equilibrium crystallization conditions produce fi ne-grained textures that feature fast rates of nucleation, highly defective substructures, smaller mosaic block size, and layered structures in cross-section. A pulsed current density amplitude of 15 to 50 A/dm² yields the best properties of coatings, including high refl ectivity and minimum porosity. The paper demonstrates that the pulse repetition frequency signifi cantly infl uences the concentration of crystal lattice defects, as well as the dislocation density and hydrogen content in coatings. Low frequencies generate a supersaturated solid hydrogen solution, leading to increased internal stresses and coating cracking. Higher pulse frequencies decrease the extent of hydrogen adsorption, resulting in more stable coating substructures and better mechanical properties. The authors have determined an optimal pulse duration at which the crystal nucleation rate exceeds the crystal growth rate, thereby promoting the formation of a fi ne-grained texture. The microhardness of coatings deposited at the optimal pulsed current parameters reaches 4 300 MPa, which is almost three times higher than in coatings deposited using direct current. Moreover, the adhesion strength of electrodeposited coatings attains 650 MPa. The coatings retain their excellent mechanical properties and low porosity after accelerated corrosion testing. Better mechanical and protective properties result from the highly defective fi ne-grained texture, a reduced content of hydrogen, and the layered coating structure. The fi ndings of the research can be used to predict the parameters of an electrodeposition process using pulsed current to apply nickel coatings to components that operate under extreme conditions, particularly components in rocket and space technologies that experience severe thermomechanical and corrosive loads.

Key words: electrodeposition, pulsed current, nickel coatings, texture, properties

Bibliography:

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19.2.2018 Control of Validity and Assessment of Accuracy of Telemetry Results during Full-Scale Test of Launch Vehicles https://journal.yuzhnoye.com/content_2018_2-en/annot_19_2_2018-en/ Thu, 07 Sep 2023 12:23:58 +0000 https://journal.yuzhnoye.com/?page_id=30801
Control of Validity and Assessment of Accuracy of Telemetry Results during Full-Scale Test of Launch Vehicles ISSN: 2617-5525 e-ISSN: 2617-5533 Authors: Aksiuta О. A., Titarenko B. A., Konstantinov G. Control of Validity and Assessment of Accuracy of Telemetry Results during Full-Scale Test of Launch Vehicles. А., Balyayev O. A., Konstantinov G. I., Sidoruk V. quot;Control of Validity and Assessment of Accuracy of Telemetry Results during Full-Scale Test of Launch Vehicles," Космическая техника. Missile armaments, vol. А., Balyayev O. A., Konstantinov G. I., Sidoruk V. quot;Control of Validity and Assessment of Accuracy of Telemetry Results during Full-Scale Test of Launch Vehicles," Космическая техника.
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19. Control of Validity and Assessment of Accuracy of Telemetry Results during Full-Scale Test of Launch Vehicles

ISSN: 2617-5525

e-ISSN: 2617-5533

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2018 (2); 157-172

DOI: https://doi.org/10.33136/stma2018.02.157

Language: Russian

Annotation: The measurement errors upon conducting flight tests for launch vehicles are evaluated by considering the interferences and uncertainties in the measurement system procedure. Formal use of this approach can lead to unpredictable consequences. More reliable evaluation of errors upon conducted measurements can be achieved if the measurement process is regarded as a procedure of successive activities for designing, manufacturing, and testing the measurement system and the rocket including measurements and their processing during the after-flight analysis of the received data. The sampling rates of the main controlled parameters are three to ten times higher than the frequency range of their changing. Therefore, it is possible to determine the characteristics of the random error components directly on the basis of registered data. The unrevealed systematic components create the basic uncertainty in the evaluation of the examined parameter’s total measurement error. To evaluate the precision and measurement accuracy of a particular launch, the article suggests specifying the preliminary data on measurement error components determined during prelaunch processing and launch. Basic structures of algorithms for evaluation of precision and measurement accuracy for certain mathematical models that form the measured parameters were considered along with the practical case when static correlation existed among the measured parameters.

Key words: flight tests, sensor, measurement error, mathematical model

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