Search Results for “Ignat’yev O. D.” – Collected book of scientific-technical articles https://journal.yuzhnoye.com Space technology. Missile armaments Fri, 22 Mar 2024 10:17:05 +0000 en-GB hourly 1 https://journal.yuzhnoye.com/wp-content/uploads/2020/11/logo_1.svg Search Results for “Ignat’yev O. D.” – Collected book of scientific-technical articles https://journal.yuzhnoye.com 32 32 5.1.2016 Scientific-Technical Base for Creation of Detonation Solid Rocket Motors https://journal.yuzhnoye.com/content_2016_1/annot_5_1_2016-en/ Tue, 23 May 2023 12:59:41 +0000 https://journal.yuzhnoye.com/?page_id=27608
2016 (1); 34-45 Language: Russian Annotation: The results of developments and investigations are presented in the field of detonation solid rocket motors (DSRM) conducted jointly by the Institute of Technical Mechanics of the National Academy of Science of Ukraine and State Space Agency of Ukraine (ITM of NASU and SSAU, hereafter ITM) and Yuzhnoye State Design Office (hereafter Yuzhnoye SDO). Missile armaments Том: 2016 Випуск: 2016 (1) Рік: 2016 Сторінки: 34—45.doi: . Missile armaments Том: 2016 Випуск: 2016 (1) Рік: 2016 Сторінки: 34—45.doi: . Missile armaments Том: 2016 Випуск: 2016 (1) Рік: 2016 Сторінки: 34—45.doi: .
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5. Scientific-Technical Base for Creation of Detonation Solid Rocket Motors

Organization:

The Institute of Technical Mechanics, Dnipro, Ukraine1; SE “PA Yuzhny Machine-Building Plant”, Dnipro, Ukraine2

Page: Kosm. teh. Raket. vooruž. 2016 (1); 34-45

Language: Russian

Annotation: The results of developments and investigations are presented in the field of detonation solid rocket motors (DSRM) conducted jointly by the Institute of Technical Mechanics of the National Academy of Science of Ukraine and State Space Agency of Ukraine (ITM of NASU and SSAU, hereafter ITM) and Yuzhnoye State Design Office (hereafter Yuzhnoye SDO). The physical basis, design peculiarities of DSRM with continuous (not pulsed) operation mode, the test base characteristics, the results of development and firing tests of DSRM test models for some space rocketry items are described. The assessments are made of achieved and prospective levels of DSRM technical characteristics, their application areas and a number of problems requiring solution.

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5.1.2016 Scientific-Technical Base for Creation of Detonation Solid Rocket Motors
5.1.2016 Scientific-Technical Base for Creation of Detonation Solid Rocket Motors
5.1.2016 Scientific-Technical Base for Creation of Detonation Solid Rocket Motors
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