1. Modernization and Automation of Temperature Calculation of Measurement Errors of Climatic Chambers for Accelerated Environmental Tests

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

Language: Russian

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

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

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2. Dehydration of Hydrocarbon Fuels by Method of Over-Saturation Drop

Salo М. P., Tereschenko K. O., Ivanitsky G. М.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (1); 6-12

https://doi.org/10.33136/stma2018.01.006

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3. The Means of Functional Suppression of Radio Electronic Facilities of Small-Size Unmanned Aerial Vehicles with Electromagnetic Radiation Focusing

Gomozov А. V., Gretskikh D. V., Demchenko A. V., Tsikalovsky M. М.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (1); 13-19

https://doi.org/10.33136/stma2018.01.013

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4. Determination of Angular Acceleration of Rotary Elements of Rocket Systems during Ground Tests

Zavialov P. P., Shatov O. А.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (1); 20-26

https://doi.org/10.33136/stma2018.01.020

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5. Experimental Determination of Lateral Force Caused by SRM Thrust Vector Eccentricity and Skew

Bezkrovny І. B., Lysenko M. T., Tregubenko О. О.

Language: Ukrainian

Kosm. teh. Raket. vooruž. 2018 (1); 27-30

https://doi.org/10.33136/stma2018.01.027

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6. On Building of Inertial Navigation System in the Condition of Presence of Considerable g-Load and Angular Velocity in Preferential Direction

Degtyareva O. А., Lapko O. M., Meleshko A. O., Chucha Y. V.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (1); 31-38

https://doi.org/10.33136/stma2018.01.031

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7. Prospective Gas Purification Device for LRE Test Bench

Sheiko А. F., Petrenko I. P., Dneprov P. Е., Ivanov S. А.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (1); 39-45

https://doi.org/10.33136/stma2018.01.039

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8. The Solid–Propellant Motors with Regulated Thrust

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

Language: Russian

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

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

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9. On the Peculiarities of High-Temperature Rocket Propellants Drain from Delivery Means to Filling Tank for Closed Drain

Pozdieiev H.L., Gamaza А. Е.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (1); 53-57

https://doi.org/10.33136/stma2018.01.053

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10. The Rocket Propellant Vapors and Water Solutions Neutralization Units. The Accumulated Experience and Prospects of Updating the Neutralization Units

Shynkorenko О. I., Starkov O. O.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (1); 58-62

https://doi.org/10.33136/stma2018.01.058

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11. Ensuring Long Lifetime of the Electrochemical Accumulators Included in Space Rocketry Electric Power Supply Systems

Zemlyanoy K. M., Reva V. S., Frolov V. P., Bezruchko K. V., Kharchenko А. А.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (1); 63-68

https://doi.org/10.33136/stma2018.01.063

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12. A Device for Soft Separation of Spacecraft from Launch Vehicle

Bondar’ М. А., Voloshin V. V., Duplischeva О. М., Mikhailov K. F., Porubaimekh V. I.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (1); 69-71

https://doi.org/10.33136/stma2018.01.069

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13. On Selection of Materials for Creation of Modern LV Thermostating System Mating Hoses

Bigun S. O., Yevchik V. S., Khorolskyi M. S.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (1); 72-84

https://doi.org/10.33136/stma2018.01.072

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14. On Selection of Materials for Creation of Modern LV Thermostating System Mating Hoses

Malyi L. P., Lavreshov V. V., Kramarenko O. M., Omelchenko D. S.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (1); 85-91

https://doi.org/10.33136/stma2018.01.085

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15. The Results of Using Automated Methods to Solve Standardization Tasks in Yuzhnoye SDO Practice

Shipko O. F., Matus G. V., Il’ina S. M., Fesenko E. Y.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (1); 91-100

https://doi.org/10.33136/stma2018.01.091

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16. Some Correlation Dependences in Families of Aton and Apollo and Rendezvous Frequency in Main Asteroid Belt

Usichenko V. I., Zavraisky D. V.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (1); 101-117

https://doi.org/10.33136/stma2018.01.101

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