Weights and sizing assessment in the context of small launcher design von ONEL, Alexandru-Iulian, CHELARU, Teodor-Viorel

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Trajectory assessment and optimisation in the context of small launcher design von ONEL, Alexandru-Iulian, CHELARU, Teodor-Viorel

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Aerodynamic assessment of axisymmetric launchers in the context of multidisciplinary optimisation von ONEL, Alexandru-Iulian, CHELARU, Teodor-Viorel

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Mathematical model of unmanned aerial vehicle used for endurance autonomous monitoring von Chelaru, Teodor-Viorel, Chelaru, Adrian

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Computational model for simulation small testing launcher, technical solution von Chelaru Teodor-Viorel, Barbu, Cristian, Chelaru Adrian

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Liquid rocket engine performance assessment in the context of small launcher optimisation von ONEL, Alexandru-Iulian, POPESCU, Oana-Iuliana, NECULAESCU, Ana-Maria, AFILIPOAE, Tudorel-Petronel, CHELARU, Teodor-Viorel

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Stability of Single-Channel Homing Rolling Aerospace Vehicle von Chelaru, Teodor-Viorel, Constantinescu, Cristian Emil, Pană, Valentin, Ene, Costin, Chelaru, Adrian

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Performance Evaluation for Launcher Testing Vehicle von Chelaru, Teodor-Viorel, Pană, Valentin, Ene, Costin

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Small Orbital Launcher - Risk Zone Evaluation von Chelaru, Teodor Viorel, Chelaru, Adrian, Onel, Alexandru Iulian

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Parametric analysis of a two-stage small launcher using a MDO approach von ONEL, Alexandru-Iulian, CHELARU, Teodor-Viorel

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Coherent solutions to roll damping derivatives evaluation for a generic rocket model von BUNESCU, Ionut, BOGOS, Stefan, CHELARU, Teodor-Viorel, HOTHAZIE, Mihai-Vladut, PRICOP, Mihai-Victor

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Hybrid rocket engine, theoretical model and experiment von Chelaru, Teodor-Viorel, Mingireanu, Florin

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Attitude Control Synthesis for Small Satellites Using Gradient Method. Part I - Nonlinear Equations von Chelaru, Teodor-Viorel, Stoica, Adrian-Mihail, Chelaru, Adrian

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Attitude Control Synthesis for Small Satellites Using Gradient Method Part II Linear Equations, Synthesis von Chelaru, Teodor-Viorel, Stoica, Adrian-Mihail, Chelaru, Adrian

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Launch Vehicle - MDO in the development of a Microlauncher von Afilipoae, Tudorel-Petronel, Neculăescu, Ana-Maria, Onel, Alexandru-Iulian, Pricop, Mihai-Victor, Marin, Alexandru, Perșinaru, Alexandru-Gabriel, Cișmilianu, Alexandru-Mihai, Munteanu, Camelia-Elena, Toader, Adrian, Sirbi, Adriana, Bennani, Samir, Chelaru, Teodor-Viorel

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Flexible Model for Miro-launcher Dynamics von Chelaru, Teodor-Viorel, Pana, Valentin, Onel, Alexandru Iulian, Afilipoae, Tudorel-Petronel, Cojocaru, Andrei Filip, Vasile, Ionut Cosmin

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Wind Influence on Miro-launcher Dynamics Model von Chelaru, Teodor-Viorel, Pana, Valentin, Onel, Alexandru Iulian, Afilipoae, Tudorel-Petronel, Cojocaru, Andrei Filip, Vasile, Ionut Cosmin

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A SOLUTION FOR GUIDANCE EQUATIONS IN THE PLANAR CASE OF HOMING MISSILES BASED ON SERIES DEVELOPMENT von Chelaru, Teodor-Viorel, Pana, Valentin

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Nonlinear Model for Micro-Launcher Attitude Control von Chelaru, Teodor-Viorel

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Performances Evaluation for Microlauncher, Mathematical Model von Chelaru, Teodor-Viorel

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