Space flight mechanics  

LEARNING OUTCOMES OF THE COURSE UNIT Learning basic principles of space flight mechanics. Acquiring knowledge of aerospace techniques (launchers, space vehicles and stations). AIMS The goal is to familiarize students with the branch of the area of aeronautical and cosmic means of transport that develops in a progressive way and with main problems of space flights. SYLLABUS 1. Historical introduction to astronautics. 2. Basic problems of space flight and its technical solutions. 3. Definition and clasification of space vehicles. Coordinate systems in mechanics of space flight. 4. Passive motion in a central gravitational field. Kepler's laws. 5. Position and velocity of cosmic bodies in orbit. Integral energy. 6. Description orbit. Orbit elements. 7. Active motion of space vehicles. Dynamics of rocket motion. 8. Flight performance of space vehicles. Specific impulse. 9. Launch of artificial Earth satellite. Characteristic of space velocities. 10. Maneuvering in orbit. Active-controlled movement of space vehicles. 11. Meeting spacecraft in orbit. 12. Interplanetary space flight. 13. Re-entry problems. EXERCISE 13 hours, compulsory TEACHER / LECTURER Ing. Jaroslav Bartoněk SYLLABUS 1. Calculations of basic parameters of the orbit in the central gravitational field. 2. Time course of motion of a cosmic body - solution of Kepler's equation. 3. Calculation of position and velocity of a body in the perifocal coordinate system. 4. Calculation of position and speed using Lagrange coefficients. 5. Position and velocity of a cosmic body in orbit in space. 6. Transformation between geocentric and perifocal coordinate system. 7. Determination of orbit elements from the state vector. 8. Calculation of the position of a body in topocentric horizontal coordinates. system. 9. Flight performance of single-stage and multi-stage missiles during vertical takeoff. 10. Coplanar changes in orbit and change in inclination of the orbit. 11. Calculation of the general transition path between two circular paths. 12. Hohmann transition path. 13. Bieliptic transition path.
Presential
English
Space flight mechanics
English

Funded by the European Union. Views and opinions expressed are however those of the author(s) only and do not necessarily reflect those of the European Union or HaDEA. Neither the European Union nor the granting authority can be held responsible for them. The statements made herein do not necessarily have the consent or agreement of the ASTRAIOS Consortium. These represent the opinion and findings of the author(s).