. "Aeronautics"@en . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . "Mechanical vibrations"@en . . "4" . "Not provided" . . "Presential"@en . "FALSE" . . "Advanced aircraft structures"@en . . "5" . "Not provided" . . "Presential"@en . "FALSE" . . "Introduction of aero elasticity"@en . . "3" . "Not provided" . . "Presential"@en . "FALSE" . . "Selective topics on space upstream"@en . . "7.5" . "Not provided" . . "Hybrid"@en . "FALSE" . . "Selective topics on space downstream"@en . . "7.5" . "Not provided" . . "Hybrid"@en . "FALSE" . . "Dynamics of flight"@en . . "4.5" . "Movement of an airplane due to gravity, engine thrust and aerodynamic forces and moments. Calculations of flight stages, distance and duration. Aircraft stability and controllability parameters and their calculation relationships.\n\nOutcome:\nAble to use aircraft motion equations to determine important maintenance characteristics at different conditions of flight. - Course work. Exam.\r\nAble to estimate static stability and controllability of an aircraft at specific conditions of flight. - Practical work. Course work. Exam.\r\nAble to estimate dynamic stability of an aircraft at short period longitudinal motion. - Practical work. Course work. Exam.\r\nAble to estimate dynamic stability of an aircraft at long period longitudinal motion. - Laboratory work. Course work. Exam.\r\nAble to demonstrate theoretical knowledge of main regularities and research methods of the dynamics of flight. Able to solve typical tasks of the dynamics of flight. - Laboratory work. Course work. Exam." . . "Presential"@en . "TRUE" . . "Aircraft maintenance and Its technical management"@en . . "6" . "The study course provides basic knowledge of aircraft maintenance management in an aviation company: organization, regulations, standards, procedures, maintenance and repair programmes.\n\nOutcome:\nKnows the basic concepts and terms of maintenance, basic knowledge of company management. - Practical work. Control work. Testing. Exam.\r\nKnows the types of aircraft maintenance, maintenance regulations. - Control work. Testing. Exam.\r\nKnows and understands PART-145 - Practical work. Control work. Testing. Exam.\r\nAble to organize aircraft maintenance and use technical means. - Control work. Testing. Exam.\r\nKnows work with technical staff. - Practical work. Control work. Testing. Exam.\r\nKnows work quality control in the field of aircraft maintenance automation. - Control work. Testing. Exam.\r\nKnows modern management methods in the field of aircraft maintenance. - Control work. Testing. Exam." . . "Presential"@en . "TRUE" . . "Modern materials and technologies in aeronautics"@en . . "6" . "During the study course, students will supplement their basic knowledge of modern materials - metal alloys, the development of their improvement techniques, as well as non-metallic materials used in aerospace, production of parts with modern additive technologies from metal and non-metallic materials. During the study course, the most characteristic materials of the aerospace industry and their properties, as well as the typical types of processing will be examined.\n\nOutcome:\nAble to obtain, select, critically evaluate and use information in the context of the study course. - Control work.\r\nAble to apply theoretical knowledge in production technology practice. - Calculations of practical work.\r\nAble to apply knowledge methods and tools for the acquisition of new knowledge and skills, development of social and professional competencies. - Control work. Laboratory works.\r\nAble to learn and apply best practices in aircraft construction and related technology areas in aircraft design. - Calculations of practical work.\r\nAble to perform technical feasibility study of the adopted design decisions. - Testing. Exam." . . "Presential"@en . "TRUE" . . "Propulsion with space applications"@en . . "7.5" . "The course covers the essentials of launchers and spacecrafts propulsion technologies, focusing on two main areas:\r\nThermal (chemistry) propulsion and electrical propulsion. The subjects treated in this course comprise performance\r\nparameters (thrust, specific impulse, etc.); Nozzle theory and thermodynamic relations; Rocket equation, staging,\r\nideal rocket theory; Solid propellant motor: components, propellants and propellant properties, performance, nozzle,\r\nthrust vectoring; Liquid propellant engine: components and subsystems, (mono- and bi-component) propellants,\r\nthrust chamber, tanks, pipes, pressure feeding systems, performance, nozzles, thrust vectoring; Cold gas thruster:\r\ncomponents and subsystems. Overview of electric propulsion systems: resistojet, ArcJet, magnetoplasmadynamic\r\nthruster, pulsed plasma thruster, ion thruster, field-emission thruster, Hall-effect thruster\n\nOutcome:\nAfter the course, the students shall be able to:\r\n• Apply the fundamental rocket theory, physical and mathematical tools to design and analyse propulsion systems\r\nfor launchers and spacecrafts.\r\n• Analyse and solve basic problems in rocket thermochemistry.\r\n• Perform preliminary design of propulsion sub-systems (thrust chambers, nozzles, tanks, etc.) for launchers and\r\nspacecrafts considering different propulsion technologies (solid, liquid and hybrid).\r\n• Execute preliminary designs of launchers and spacecrafts.\r\n• Analyse and solve basic problems in electric propulsion.\r\n• Apply the above-described techniques on real-world space vehicle projects, and report on this work both orally\r\nand in writing." . . "Presential"@en . "TRUE" . . "Introduction to aerospace engineering"@en . . "7" . "no data" . . "Presential"@en . "TRUE" . . "Aeronautical safety systems and investigations"@en . . "3" . "Aviation safety principles. Accident causation, epidemiologic model, functional resonance model. \r\nSafety culture, production – protection dilemma, safety space. Hazards and risks, consequences, risk \r\nevaluation matrix. Risk management, cost-benefit analysis. Safety Management Systems, \r\nrequirements and frames for SSP and SMS. Acceptability levels. Statistics in safety. Safety \r\ninvestigation, authorities, responsibilities, procedures, participants. Investigation techniques, clues \r\nat the crash site. Data analysis, selection of hypotheses and check, investigation reporting\n\nOutcome: Not Provided" . . "Presential"@en . "TRUE" . . "Structural and vibrational analysis and design"@en . . "8" . "no data" . . "Presential"@en . "TRUE" . . "Propulsion systems"@en . . "5" . "Learning outcomes of the course unit:\nStudent will be able to mathematically describe physical processes in different types of rocket propulsion systems. He will be able to analyze chemical rocket propulsion systems from the viewpoint of thermodynamics and fluid flow in engines and motors. Student will be able to analyze the performance characteristics of rocket engines with different input parameters as well as in different ambient conditions. Student will be able to analyze the physical parameters of the working fluid using a computational fluid dynamics (CFD). Student will gain knowledge of the design of various types of electric rocket propulsion as well as their deployment in different types of space systems. Course Contents:\nClassification of different types of rocket propulsion systems.\nChemical rocket propulsion (overview, main types and uses).\nBasic flow equations and thermodynamics of gases.\nIsoentropic flow and nozzle flow.\nPerformance characteristics of chemical rocket engines (according to individual types).\nRocket engines for liquid and solid fuel.\nCFD simulation.\nElectromagnetic rocket propulsion (overview, main types and uses).\nPhysical principles of operation and reasons for the use of electromagnetic propulsion systems.\nPerformance characteristics of electromagnetic rocket motors (according to individual types).\nMain structural elements of electromagnetic rocket motors.\nExamples of practical use of electromagnetic drive systems." . . "Presential"@en . "FALSE" . . "Aircraft systems technologies and simulation lab"@en . . "12" . "The aim of the course is to provide fundamental methods and tools for the design and analysis of the main systems employed on aircrafts for the generation, the conversion, the regulation, the distribution and the use of energy and data. All the examined systems are described in terms of general architecture and working principle, and basic design practices are also presented for relevant cases, by using reduced-order analytical models. Specific sections of the course are dedicated to the reliability/safety analysis of onboard systems, as well as to the development of numerical codes for the simulation of systems' dynamics." . . "Presential"@en . "TRUE" . . "Numerical modelling of aeronautical components"@en . . "6" . "Learning outcomes\n\nThe course describes the fundamentals of the mathematical and geometrical methodologies for the setting-up of computation models to represent the geometry of complex and free shape objects. The theoretical and practical elements to model curves and surfaces by CAD tools are given." . . "Presential"@en . "FALSE" . . "Complements of aircraft systems"@en . . "6" . "The course aims to complete the general framework of the main on-board systems necessary for the operation of an aircraft, compared to what has already been illustrated in the Aircraft Systems course. The main airport systems, required for ground operations, are also described. For each system, the operating principle is described and for some of them simple analytical tools are provided for a preliminary design." . . "Presential"@en . "FALSE" . . "Aircraft materials"@en . . "2" . "Requirements for aircraft construction materials. Strength, techno-\nlogical (formability, heat treatment, joining methods) and" . . "Presential"@en . "TRUE" . . "Aircraft maintenance engineering"@en . . "3" . "Aircraft as an object of operation. Operation strategies. Organisa-\ntion of aircraft operations. Standardisation of aircraft operation pro-\ncess. Probability of service in airworthiness. Operation definitions\nand methods. Major components of operation system structure and\nselection criteria. Structure of safe working life. Passenger aircraft\noperation. Operational safety factors of flights." . . "Presential"@en . "TRUE" . . "Aircraft construction and installation"@en . . "7" . "Aircraft requirements and classification. Forces on aircrafts and hel-\nicopters. Static and dynamic loads. Overload factor, disposable\noverload, limitations. Selection of layout and basic airframe param-\neters, statistical factors. Wing structure and its components. Work\nof girder, semi-shell, shell structures. Structure and work of the wing\nnear the recess, nodes and connections. Wing mechanisation. Ai-\nlerons, empennage and control system. Fuselage and flight deck.\nLanding gear, characteristics and classification, landing gear re-\nquirements. Main and auxiliary landing gear design, suspension,\nairwheel design. Selection of layout and basic parameters of heli-\ncopter airframe. Lift rotor requirements; types and parameters" . . "Presential"@en . "FALSE" . . "Basics of propulsion systems"@en . . "4" . "Thermodynamic state. The equations of state of perfect and real\ngases. Properties of gas mixtures. Principles of thermodynamics.\nCharacteristic transformations. Thermodynamic circuits. Funda-\nmentals of flow thermodynamics. Heat transfer: conduction, con-\nvection and radiation. Theoretical fundamentals of piston engines.\nTheoretical fundamentals of single and dual flow turbine jet engines\nand propeller turbine engines. Theoretical fundamentals of jet en-\ngines. Fundamentals of aeroplane propulsion systems (jet, helicop-\nter and propeller) with piston and turbine engines. Basic engine sys-\ntems (oiling, power, starting and ignition). Hydromechanical and\nelectronic control systems (FADEC). Engine parameter display\nsystems." . . "Presential"@en . "FALSE" . . "Aircraft measurement and diagnostic systems"@en . . "5" . "Classification of aircraft measuring instruments and systems.\nAircraft Traffic Environment. International Standard Atmosphere.\nOn-board installation of air pressure receivers. Aerometric Switch-\nboards. Angle of attack and glide sensors. Accelerometers and stall\ntransmitters. Aircraft heading measurement. Magnetic and induc-\ntive compasses. Theory and classification of gyroscopes. Review\nand characterisation of aeronautical gyroscopes. Characteristics of\naeronautical gyroscopic instruments and systems. Measurement\nand indication of engine exhaust gas temperature. Measurement\nand indication of rotational speed of engine rotors. Measurement\nand indication of pressure, fuel quantity and flow rate. Measure-\nment and indication of other engine operating parameters (vibra-\ntions, position of control bodies, unsteady compressor operation,\netc.). Essence of technical diagnostics. Basic terms and terminol-\nogy. Diagnostic signals and parameters. Diagnostic models. Diag-\nnostic algorithms. Diagnostic methods and equipment. Expert sys-\ntems in diagnostic inference process. Artificial neural networks in\ndiagnostic systems. Overview of design solutions for measurement\ncircuits and systems of selected aircraft used in the Polish Armed\nForces." . . "Presential"@en . "FALSE" . . "Aircraft power systems"@en . . "4" . "Classification of on-board electrical and energy systems (PUEE).\nAircraft accumulator batteries. Aircraft DC generators. Aircraft gen-\nerators of alternating current. Secondary sources of electrical\npower. On-board electrical power systems and their components.\nStructures of electrical power systems in a state of inoperability. El-\nements of on-board transmission and distribution systems. Light\nsignalling systems. Fire-fighting and anti-icing systems. Aircraft en-\ngine ignition systems." . . "Presential"@en . "FALSE" . . "On-board visualization systems and simulators"@en . . "5" . "Evolution of aeronautical information imaging systems. Examples\nof instrument layout in the cockpit. Perception of information, char-\nacteristics of pilot-operator receptors. Elements of aeronautical er-\ngonomics. Electronic indicators. Computer-based information im-\naging systems. Construction and principle of operation of cathode" . . "Presential"@en . "FALSE" . . "Theory of aircraft engines"@en . . "5" . "Operating principles of an aircraft piston engine and their charac-\nteristics. Operating parameters of a single-flow turbine jet engine.\nTwo-flow turbine jet engine and its application. Propeller and heli-\ncopter turbine engine. Parameters and operating characteristics of\ncomponents (inlet, compressor, combustion chamber, turbine and\ntypes of exhaust systems in turbine engines). Basic characteristics\nof turbine engines. Analysis of engine characteristics linking engine\nparameters to flight parameters. Conclusions resulting from the\nanalysis of fundamental importance to the problems of construction\nand operation of aircraft engines." . . "Presential"@en . "FALSE" . . "Strength of aircraft structures"@en . . "5" . "General information. Girders. Membrane theory of cylindrical\nshells. Free torsion of thin-walled prismatic bars. Open section\nbending and shearing of thin-walled bars. Bending and shear of\nthin-walled bars with closed cross-section. Sandwich construction\n(three layer construction). Elastic stability of bars. Elastic stability of\nplates. Structural work after loss of stability. Current directions of\ndevelopment of strength calculation methods for aeronautical struc-\ntures." . . "Presential"@en . "FALSE" . . "Aircraft structure design"@en . . "8" . "Aircraft requirements and classification. Selection of layout\nand basic airframe parameters, statistical factors. Construction of\nwing and its components. Work construction: girder, semi-shell,\ncrust. Structure construction and operation of the wing near the\nwingtip, nodes and connections. Wing mechanisation. Ailerons,\nempennage and control system. Fuselage and flight deck. Landing\ngear, characteristics and classification, landing gear requirements.\nMain and auxiliary landing gear design, suspension, airwheel" . . "Presential"@en . "FALSE" . . "Aircraft propulsion systems"@en . . "4" . "Construction of aircraft propulsion systems with turbine engines\n(jet, propeller and helicopter) and piston engines; construction,\nloads and strength calculations of basic engine units and their parts;\nconstruction materials; engine installations - construction and prin-\nciples of operation, structure and operation of individual units, pro-\npellants and lubricants; hydro-mechanical and electronic control\nsystems; reduction gearing of aircraft engines; propeller construc-\ntion, propeller pitch control; inlet air dust collectors; starting of tur-\nbine and piston engines; operation and diagnosis of aircraft propul-\nsion systems; indication of operational parameters of propulsion\nsystems." . . "Presential"@en . "FALSE" . . "Design and manufacture of aircraft structures"@en . . "4" . "Specificity of the airframe as a production object. Methods of map-\nping airframe geometry. Methods of shaping parts from thin sheets\nand sections. Methods of manufacturing integral metal and compo-\nsite parts. Connection technologies used in the assembly of parts\nand subassemblies of airframes (riveting, bonding, gluing). Sub-as-\nsembly and final assembly. Methods of assuring quality and relia-\nbility of parts. Aircraft wear and damage. Capabilities\nand technologies for the repair of airframe coverings and strength\nmembers. Repairs of sandwich and composite structures." . . "Presential"@en . "FALSE" . . "Theory of aircraft engines"@en . . "5" . "Operating principles of an aircraft piston engine and their charac-\nteristics. Operating parameters of a single-flow turbine jet engine.\nTwo-flow turbine jet engine and its application. Propeller and heli-\ncopter turbine engine. Performance and characteristics of compo-\nnents (inlet, compressor, combustion chamber, turbine and types\nof exhaust systems in turbine engines). Basic characteristics of tur-\nbine engines. Analysis of engine characteristics linking engine pa-\nrameters to flight parameters. Conclusions resulting from the anal-\nysis of fundamental importance to the problems of construction and\noperation of aircraft engines." . . "Presential"@en . "FALSE" . . "Strength of aircraft structure"@en . . "5" . "General information. Girders. Membrane theory of cylindrical\nshells. Free torsion of thin-walled prismatic bars. Bending and\nshearing of thin-walled bars with open section. Bending and shear\nof thin-walled bars with closed section. Sandwich construction\n(three layer construction). Elastic stability of bars. Elastic stability of\nplates. Structural work after loss of stability. Current development\ntrends of strength calculation methods for aeronautical structures." . . "Presential"@en . "FALSE" . . "Aircraft construction"@en . . "4" . "Evolution of aircrafts and helicopters design, classifications. Forces\noperating on airplane and helicopter. Static and dynamic loads.\nOverload factor, disposable overload, limitations. Load curve. Wing\nand rotor blade loads. Loads on ailerons, flaps and spoilers and\ncontrol system. Fuselage and landing gear loads. Design trend\nanalysis. Preliminary mass estimation. Wing, blade, fuselage, land-\ning gear, mechanisation elements of control systems. Airframe and\npropulsion system interaction." . . "Presential"@en . "FALSE" . . "Aircraft propulsion systems"@en . . "8" . "Construction of aircraft propulsion systems with turbine engines\n(jet, propeller and helicopter) and piston engines; construction," . . "Presential"@en . "FALSE" . . "Aircraft fuels and lubricants"@en . . "1" . "General information about fuels and lubricants. Aviation fuels -\nmethods of obtaining, properties, energy characteristics. Combus-\ntion process of hydrocarbon fuels. Basic fuel combustion reactions.\nAviation fuels - basic characteristics, normative requirements, as-\nsortment range and principles of use. Additives to aviation fuels.\nMethods of assessing resistance to knocking combustion. Fuels for\naviation turbine engines - basic characteristics, normative require-\nments, assortment range and principles of use. Fuel additives. Air-\nport control of fuel quality. Deposits and smoking. Malfunctions of\naviation turbine engines related to fuel quality. Lubricating oils used\nin aviation - basic characteristics, normative requirements, range\nand principles of use. Greases, technical and auxiliary fluids used\nin aviation. Transport, storage and distribution of fuels and lubri-\ncants." . . "Presential"@en . "FALSE" . . "Aircraft power supply systems"@en . . "6" . "no data" . . "Presential"@en . "FALSE" . . "Mechanical vibrations"@en . . "4" . "no data" . . "Presential"@en . "FALSE" . . "Advanced aircraft structures"@en . . "5" . "no data" . . "Presential"@en . "FALSE" . . "Introduction of aero elasticity"@en . . "3" . "Influence of aeroelasticity phenomena over aircraft stability and controllability characteristics." . . "Presential"@en . "FALSE" . . "Aircraft propulsion"@en . . "no data" . "This module introduces students with the basics of aircraft propulsion systems. It will provide an understanding of the different propulsion systems for subsonic and supersonic flight and understanding of performance parameters of air breathing engines." . . "Presential"@en . "TRUE" . . "Aircraft propulsion"@en . . "no data" . "Anotation:\r\n\r\nThis course gives basic knowledge of the aircraft propulsion theory, thermal cycles of aircraft powerplants and basics of aero- and thermodynamics of aircraft powerplants components. The influence of design parameters on propulsion system efficiency, specific fuel consumption and thrust is analyzed for the given flight velocity. Design layouts of the aerospace propulsion units are introduced and function of their components is described. The focus is given on the comparison of various systems and the choose of the appropriate one. Enviromental aspects are mentioned together with the common and alternative fuels and energy sources.\r\nStudy targets:\r\n\r\nThe goal of study is the description of the enegetical transformation in aerospace propulsion systems and their properties.\r\nCourse outlines:\r\n\r\n1.\t \tHistorical overview, forces acting on an aircraft, thrust, power, efficiency\r\n2.\t \tPropulsion systems, their thrust and power\r\n3.\t \tPropeller, basic aerodynamics, thrust, power, efficiency and dimensionless parameters\r\n4.\t \tApplied thermodynamics and aerodynamics\r\n5.\t \tAircraft piston engines\r\n6.\t \tTurbine engines\r\n7.\t \tBasics of the turbomachinery aerodynamics\r\n8.\t \tAxial and radial compressors\r\n9.\t \tTurbines for aircraft powerplants\r\n10.\t \tIntake ducts and nozzles\r\n11.\t \tCombustion chambers\r\n12.\t \tTurbojet, turbofan and turboprop engines\r\n13.\t \tDependence of powerplant characteristics on the flight velocity and altitute\r\n14.\t \tNoise and enviromental issues of aircraft powerplants\r\nExercises outline:\r\n\r\nExcercises are focused on the practising of computational methods which were explained during lectures. Basic methods are used to determine thrust, power and efficiency for aircraft powerplants and propellers. Advantages and disadvantages of various propulsion systems are analyzed and compared. Results are discussed in order to obtain theoretical background for choosing of the appropriate propulsion system for given aircraft." . . "no data"@en . "TRUE" . . "Aircraft structures and materials"@en . . "no data" . "Anotation:\r\n\r\nThe course is an introduction lecture for structure branch aerospace technologyavionics and air trafics. The course acquaints with fundamental types of aircraft structures, forces acting on the aircraft structures and aircraft materials. It further acquaints with functions of aircraft control surfaces. Philosophy of the safety, reliability, strength certification, and airworthiness as well as the aviation regulations is given.\r\nStudy targets:\r\n\r\nThe goal of the course is get to know and understand fundamentals of aircraft structures. It represents an understanding of philosophy of an aircraft structure design (types of structures, loads, structure limit states, ...) in relation to the safety, reliability and certifications required by the aviation regulations.\r\nCourse outlines:\r\n\r\n1.\t \tHistory and development of aeronautics.\r\n2.\t \tDesign philosophy and role of certification specifications.\r\n3.\t \tSafety, reliability and airworthiness.\r\n4.\t \tLoading of aircraft and load factor.\r\n5.\t \tManoeuvring loads. Manoeuvring envelope of load factor.\r\n6.\t \tGust load. Gust envelope and envelope of limit load factor.\r\n7.\t \tMass of aircraft, centre of gravity position, mass envelope.\r\n8.\t \tClassification of aircraft. Fundamental parts and systems.\r\n9.\t \tFundamental parts of airframe, aircraft materials and loading distribution on the structure.\r\n10.\t \tWing construction.\r\n11.\t \tLift and drag devices.\r\n12.\t \tFuselage construction.\r\n13.\t \tEmpennage construction.\r\n14.\t \tUndercarriage\r\nExercises outline:\nIn the introductory part, the exercises will be focused on practical exercises of the state relations between the quantities of the international standard atmosphere and the calculation of basic aerodynamic force effects. Furthermore, they will introduce the content of building regulations and the way they are used in load design (flight envelopes of operational multiples) according to a specific category of aircraft. In the final part, the assembly of the mass envelope and the methodology of the airframe certificate will be practiced by numerical strength control of selected parts of the airframe (beam, cavity, strut). Excursions will also be organized as part of the exercise with practical examples of testing aircraft structures." . . "no data"@en . "TRUE" . . "Experimental methods in aeronautics"@en . . "no data" . "Anotation:\n\nIntroduction to the basic methods of measuring non-electrical quantities, procedures for conducting engineering experiments, evaluation and processing of data. Introduction to basic methods of aircraft specifics testing. Processing of individual labs and practical demonstrations of experimental techniques and procedures.\nStudy targets:\n\nIntroduction to basic methods of aircraft specifics testing.\nCourse outlines:\n\n1. Motivational first introduction, overview of quantities, dimensional analysis, the organization of the experiment, safety, accuracy of measurement, uncertainty, the comparison of results of experiments and calculations\n2. Data aquisition software for experiment control and data processing, basic instrumentation\n3. Analog and digital signal processing, signal filtering\n4. Sensors for measuring non-electrical values\n5. Aerodynamics - tunnel force measurement, pressure measurement\n6. Mechanics - strain gauge analysis\n7. Mechanics - specifics of testing aircraft materials and assemblies, strength testing, buckling\n8. Mechanics - Stress tests of aircraft structures, fatigue\n9. Climatic resistance\n10. Measurement of vibration and noise, experimental modal test, aeroelasticity\n11. Flight Tests\n12. Excursion - strength and fatigue testing\n13. Excursion - testing of turbine engines\n14. Evolution of aircraft structures testing methods\nExercises outline:\n\n1. Aerodynamics - basic pressure measurements\n2. Aerodynamics - advanced measurements of flow fields\n3. Strength - determination of basic strength properties of materials\n4. Strength - application of strain gauges\n5. Modal analysis\n6. Noise\n7. Nondestructive testing of structures" . . "no data"@en . "TRUE" . . "Aeronautical systems 1"@en . . "3" . "Thepresentation of basics of aeronautical systems: principles of operation and applications" . . "Presential"@en . "TRUE" . . "Introduction to aerospace"@en . . "2" . "Basic knowledge about history of avaiation\n Knowledge of present problems of avaiation\n Knowledge of basic terms on aeronautical technology. fter subject is completed student should have the basic knowledge on:\n • the history of aviation,\n • present problems of aviation,\n • basic terms on aeronautics and aircraft technology." . . "Presential"@en . "TRUE" . . "Hybrid propulsion and new launch systems"@en . . "6" . "Definition of propulsion by rocket : static performance of rockets for launch to space missions ; definition of thrust and drag ; equation of motion of a rocket ; state variables and control ; constraints on the trajectory . Performance of single\u0002stage and multistage rocket . Definition of thrust requirements for performing space missions. Definition and \r\nclassification of Propellants for hybrid engines. Process Combustion : subsonic combustion . Influence of the initial conditions of the propellant . Calculation of the temperature of combustion in conditions of chemical equilibrium. \r\nSizing and design procedures for (a) Injection system (injectors), (b) nozzle, (c) thrust chamber. New launch systems: \r\n(a) gun launch to orbit ( ram accelerator and railgun ), (b) launch from aircraft in subsonic flight, (c) airbreathing SSTO \r\nlaunch vehicles." . .