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Browsing by Author Miloš, Marko
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| Issue Date | Title | Author(s) | Type | Мp-cat. |
|---|---|---|---|---|
| 2012 | 6 DOF Thrust Vector Control Test Stand Based on Stewart Platform Design | Branislav Jojić; Đorđe Blagojević; Miloš, Marko | Conference Paper | Mp. category will be shown later |
| 2015 | A novel 6 dof thrust vector control test stand![]() | Predrag, Miloš; Davidović, Nikola; Jojić, Branislav | Article | 22M22 |
| 2022 | Analysis and design of the gas generator multifunctional bulkhead considering the thermal and structural loads | Kolarević, Nenad | Article | 22M22 |
| 2009 | Analysis of thermoplastic propellants and their ingredients with DSC and tga | Bozić, V.S.; Krakovsky, I.; Miloš, Marko | Article | Mp. category will be shown later |
| 2010 | Application of Thermoplastic Composite Propellants in Production of Propellant Grains and Rocket Motors | Miloš, Marko | Conference Paper | Mp. category will be shown later |
| 2014 | Asistirani inercijalni navigacioni sistem – AINS v1.0 | Branislav Jojić; Miloš, Marko | Technical reports | Mp. category will be shown later |
| 2018 | Биомимикрија као метод аеродинамичког дизајнирања воза великих брзина![]() | Linić, Suzana Lj. | Doctoral theses | 70M70 |
| 2017 | Cascade nonlinear feedforward-feedback control of stagnation pressure in a supersonic blowdown wind tunnel | Ilić, Biljana | Article | 21M21 |
| 2010 | Composite Rocket Propellants Based on Thermoplastic Elastomer Binders | Miloš, Marko | Conference Paper | Mp. category will be shown later |
| 2010 | Control of Electro-Mechanical Actuator for Aerospace Applications![]() | Khan, Muhammad Ashraf | Article | 23M23 |
| 2018 | Crucial parameters of gas generator on tip-jet helicopter | Kolarević, Nenad | Conference Paper | Mp. category will be shown later |
| 2013 | Kriterijumi za izbor odgovarajućeg algoritma upravljanja elektro-hidrauličnog aktuatora primenjenog na raketnom motoru sa pokretnim mlaznikom i pod specifičnim opterećenjem | Dragan Nauparac; Pršić, Dragan | Article | 24M24 |
| 2012 | Design Criterion To Select Adequate Control Algorithm For Electro-Hydraulic Actuator Applied To Rocket Engine Flexible Nozzle Thrust Vector Control Under Specific Load | D. Nauparac; Pršić, Dragan | Article | 24M24 |
| 2018 | Design of electro-mechanical actuator for medium sized helicopter and a test platform for its testing and verification![]() | Tanasković Marko | Conference Paper | Mp. category will be shown later |
| 2011 | Design selection of adequate control algorithm for electro-hydraulic actuator applied on rocket engine flexible nozzle thrust vector control | D. Nauparac; Pršić, Dragan | Conference Paper | Mp. category will be shown later |
| 2020 | Design Solution and Structural Optimisation of Feathering Hinge Assembly of Teetering Rotor Head for Tip-Jet Helicopters | Kolarević, Nenad | Conference Paper | Mp. category will be shown later |
| 2015 | Different modeling technologies of hydraulic load simulator for thrust vector control actuator![]() | Nauparac, Dragan B.; Pršić, Dragan | Article | 22M22 |
| 2018 | Dynamic stability of high speed turboshaft engine with reducer | Kolarević, Nenad | Conference Paper | Mp. category will be shown later |
| 2001 | Effects of oxidizer particle size on propellants based on modified polyvinyl chloride | Bozić, V.S.; Miloš, Marko | Article | 21M21 |
| 2012 | Electro-Hydraulic System for the Simulation of Dynamic Behaviour of Rocket Engine Flexible Nozzle Thrust Vector Control | D. Nauparac; Pršić, Dragan | Conference Paper | Mp. category will be shown later |
