7.1.2017 Static Approach Application in Analysis of Gas-Dynamic Parameters in Launch Vehicle Vented Bays

Static Approach Application in Analysis of Gas-Dynamic Parameters in Launch Vehicle Vented Bays ISSN: 2617-5525 e-ISSN: 2617-5533 Authors: Sirenko V. 2017 (1); 43-47 [...]

9.1.2017 Mathematical Simulation of Gas-Jet Control System Distributor for Launch Vehicles

Mathematical Simulation of Gas-Jet Control System Distributor for Launch Vehicles ISSN: 2617-5525 e-ISSN: 2617-5533 Authors: Oliinyk V. 2017 (1); 59-66 Language: Russian [...]

11.2.2016 Experimental Investigation into Power Characteristics of Fast-Flowrate Gas Jet Propulsion Systems

Experimental Investigation into Power Characteristics of Fast-Flowrate Gas Jet Propulsion Systems ISSN: 2617-5525 e-ISSN: 2617-5533 Authors: Anishchenko V. 2016 (2); 72-74 [...]

6.1.2019 Investigation into Peculiarities of Delivery to Launch Base of Rocket Propellant with Specified Gasing

Investigation into Peculiarities of Delivery to Launch Base of Rocket Propellant with Specified Gasing ISSN: 2617-5525 e-ISSN: 2617-5533 Authors: Pozdieiev H. Knowing the [...]

24.1.2019 Porous Cast Materials (Gasars). Options of Their Use in Space Rocket Hardware

Porous Cast Materials (Gasars). 2019, (1); 163-170 DOI: https://doi.org/10.33136/stma2019.01.163 Language: Russian Annotation: Gasars is a new type of porous cast [...]

23.1.2019 Calculation of Thermal-Physical Properties of Gaseous Xenon

Calculation of Thermal-Physical Properties of Gaseous Xenon ISSN: 2617-5525 e-ISSN: 2617-5533 Authors: Kravchenko N. 2019, (1); 154-162 DOI: [...]

13.1.2016 The Impact of Diaphragm’s Shape on Gas Dynamic Flow Characteristics in Small-Size SRM Combustion Chamber

The Impact of Diaphragm’s Shape on Gas Dynamic Flow Characteristics in Small-Size SRM Combustion Chamber ISSN: 2617-5525 e-ISSN: 2617-5533 Authors: Vakhromov V. (2016) [...]

6.2.2019 Stabilization of gas reducers adjustment

Stabilization of gas reducers adjustment ISSN: 2617-5525 e-ISSN: 2617-5533 Authors: Nazarenko O. 2019, (2); 42-49 DOI: https://doi.org/10.33136/stma2019.02.042 Language: [...]

5.2.2025 Analysis and minimization of resistive forces occurring during rocket stage separation. Possibility of using a single pneumatic pusher for stage separation

Based on the results of resolving an optimization problem, the utilization of one pneumatic pusher for stage separation is one of the optimum scenarios, which will enable a several [...]

3.2.2025 Electric thrusters utilizing metal plasma

A metal plasma engine does not require gas or liquid fuel, neutralizers, heaters, highvoltage electronics, or strong electric or magnetic fi elds to operate. No gases [...]