Course information

Responsible Instructor
Name E-mail
Dr.ir. M. Voskuijl    M.Voskuijl@tudelft.nl
Instructor
Name E-mail
Ir. R. Noomen    R.Noomen@tudelft.nl
Contact Hours / Week x/x/x/x
0/0/4/0
Education Period
 3
Start Education
 3
Exam Period
 3 4
Course Language
 English
Course Contents
1. Turning performance (three dimensional equations of motion, coordinate systems, Euler angles, transformation matrices)
2. Airfield performance (take-off and landing)
3. Unsteady climb and descent (including minimum time to climb problem)
4. Cruise flight and transport performance
5. Equations of motion with a wind gradient present
6. Equations of motion applied to various phases of space flight
7. Launch, Vertical flight, delta-V budget, burn out height, staging
8. Gravity perturbations to satellite orbits, J2 effect for low earth orbit satellites, J2,2 effect for Geostationary Earth Orbit sattelites leading to contribution in ïV budget
9. Patched conics approach for interplanetary flight, gravity assist effect / options for change of excess velocity (2d, 3d), Launch, in orbit insertion.
Study Goals
1. Integrate fundamental disciplines (aero, power and propulsion, mechanics..) to describe the kinematics of aerospace vehicles satisfying real world constraints
2. Derive equations of motion for elementary flight and mission phases (climb, turn, cruise, take-off, launch, orbit)
3. Derive analytical expressions for optimal performance (steepest turn, Breguet Range, patched conics, J2, maneuvers )
4. Determine pros/cons of multi-stage launchers.
5. Assess sun lighting conditions on a satellite.
6. Determine the influence of wind (gradient) on aircraft motion and performance.
7. Develop the theory to describe an interplanetary trajectory as a succession of two-body problems, and apply this concept to real missions.
Education Method
Lecturing and self study.
Literature and Study Materials
G.J.J. Ruijgrok, "Elements of Airplane Performance," 2nd Edition, VSSD (mandatory).

Fortescue, P., J. Stark and G. Swinerd: Spacecraft Systems Engineering (3rd edition), Wiley & Sons, 2003. (For further reading, not mandatory)

Wertz, J.R., and W.J. Larson: Space Mission Analysis and Design (3rd edition), Space Technology Library/Microcosm/Kluwer, 1999. (For further reading, not mandatory).
Assessment
Students do a final exam in which they get a mix of open and multiple choice questions. They have to show knowledge and insight and they have to make calculations and analytical derivations.
Set-up
Students will follow an active lecture, in a large group. The lectures will consist of a mixture of introduction of the theory, derivations, example questions and interaction with students.