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Modeling Heat Strength Characteristics of Structural Elements of a Solid Propellant Rocket Engine Manufactured Using Prototyping
| Authors: Ushakova E.S., Arefyev K.Yu., Polyanskiy A.R. | Published: 28.04.2018 |
| Published in issue: #4(697)/2018 | |
| Category: Aviation, Rocket and Technology | |
| Keywords: powder prototyping technology, safety factor, temperature conditions of the structure, convective heat transfer, nozzle block |
