Search Results for “Husev V. V.” – Collected book of scientific-technical articles https://journal.yuzhnoye.com Space technology. Missile armaments Tue, 02 Apr 2024 08:02:23 +0000 en-GB hourly 1 https://journal.yuzhnoye.com/wp-content/uploads/2020/11/logo_1.svg Search Results for “Husev V. V.” – Collected book of scientific-technical articles https://journal.yuzhnoye.com 32 32 23.2.2017 Optimization Technique for Mass of Locally Loaded Rocket Bays with Wafer Structure https://journal.yuzhnoye.com/content_2017_2/annot_23_2_2017-en/ Wed, 09 Aug 2023 12:39:28 +0000 https://journal.yuzhnoye.com/?page_id=29948
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23. Optimization Technique for Mass of Locally Loaded Rocket Bays with Wafer Structure

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2017 (2); 131-136

Language: Russian

Annotation: The paper addresses a new, authors- developed method of mass optimization of rocket bays of wafer structure bearing during operation on locally disposed parking supports. The method allows, due to more rational distribution of materials in the structure in accordance with acting load, decreasing the mass of bays by up to 20%.

Key words:

Bibliography:
1. Linnik A. K. Designing of Liquid Ballistic Missiles Cases. Dnepropetrovsk, 1994. P. 65-66.
2. Lizin V. T., Pyatkin V. A. Designing of Thin-Wall Structures. М., 1985. P. 14, 93.
3. Dzhur E. A., Vdovin S. I. et al. Space Rockets Manufacturing Technology. Dnepropetrovsk, 1992. P. 35, 36.
4. Patent 112339 Ukraine, MPK FD2 K 9/32 (2006.1), FD2 K 9/60 (2006/1), ВG4 G 1/22 (2006.1). Method of Manufacturing Lightweight Prints of Locally Loaded Wafer Structure / V. G. Danchenko, E. I. Shevtsov, V. V. Gusev (Ukraine); Applicant and holder Yuzhnoye SDO. No. а 201408785; Claimed 04.08.2014; Published 25.08.2016, Bulletin No. 16.
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23.2.2017 Optimization Technique for Mass of Locally Loaded Rocket Bays with Wafer Structure
23.2.2017 Optimization Technique for Mass of Locally Loaded Rocket Bays with Wafer Structure
23.2.2017 Optimization Technique for Mass of Locally Loaded Rocket Bays with Wafer Structure
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21.2.2017 Mass Parameter Optimization of Thermal Protective Structure for Reusable Spacecraft https://journal.yuzhnoye.com/content_2017_2/annot_21_2_2017-en/ Wed, 09 Aug 2023 12:32:56 +0000 https://journal.yuzhnoye.com/?page_id=29940
1 , Husev V. I., Husev V. I., Husev V. I., Husev V. I., Husev V. I., Husev V. I., Husev V.
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21. Mass Parameter Optimization of Thermal Protective Structure for Reusable Spacecraft

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine1; Oles Honchar Dnipro National University, Dnipro, Ukraine2

Page: Kosm. teh. Raket. vooruž. 2017 (2); 121-126

Language: Russian

Annotation: The paper considers the TZS-U design developed by Yuzhnoye SDO specialists for windward part of reusable spacecraft with external metal three-layer panel, U-like joint and tiled thermal protection, in which the problem is solved of compensation of thermal expansions and sealing of gaps; for optimization of structural mass. The specially created dispersion-hardened powder alloy based on nichrome and aluminum with yttrium dioxide with decreased specific mass of 7500 kg/m3 and lighter felt of MKRF brand are used , and honeycomb filler of three-layer panel is replaced by the filler with square cell.

Key words:

Bibliography:
1. Aerothermal performance and structural integrity of a René-41 thermal protection system at Mach 6.6 / W. D. Deveikis, R. Miserentino, I. Weinstein, J. L. Schideler. NASA-TN-D-7943, NASA, Washington DC. 1975. 105 р.
2. Poteet C. C., Blosser M. L. Improving Metallic Thermal-Protection-System Hypervelocity Impact Resistance Through Numerical Simulation. Journal of Spacecraft and Rockets. 2004. Vol. 41, No. 2. Р. 221-232.
3. Advanced metallic thermal protection system development / M. L. Blosser, R. R. Chen, I. H. Schmidt et al. AIAA-2002-0504; AIAA, Washington DC. 2002. 56 р.
4. David E. European Directions for Hypersonic Thermal Protection Systems and Hot Structures. 31st Annual Conference on Composite Materials and Structures (Daytona Beach, FL, January 22, 2007). 44 р.
5. Gusarova I. A. Selection of Scheme of Heat Protection Tile Attachment to Reusable Spacecraft Body. Problems of Designing and Manufacturing Flying Vehicle Structures. 2016. No. 4 (88). P. 105-113.
6. Gusarova I. A. Evaluation of Thermal Resistance of Three-Layer Honeycomb Panel Produced from YuIPM-1200 Alloy by Method of Diffusion Welding in Vacuum / I. A. Gusarova, М. Parko, А. М. Potapov, Y. V. Fal’chenko, L. V. Petrushinets, Т. V. Melnichenko, V. E. Fedorchuk. Automatic Welding. 2016. No. 12 (759). P. 31-35.
7. Patent 108096 Ukraine. Method of Producing Heat-Resistant Alloy Based on Nichrome / V. V. Skorokhod, V. P. Solntsev, G. O. Frolov, Т. O. Solntseva, О. М. Potapov, V. G. Tikhiy, I. A. Gusarova, Y. M. Litvinenko / Application No. а2012 11691; Claimed 04.10.2012; Published 25.03.2015, Bulletin No. 6. 4 p.
Downloads: 38
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21.2.2017 Mass Parameter Optimization of Thermal Protective Structure for Reusable Spacecraft
21.2.2017 Mass Parameter Optimization of Thermal Protective Structure for Reusable Spacecraft
21.2.2017 Mass Parameter Optimization of Thermal Protective Structure for Reusable Spacecraft
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