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Technische Universität München

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Earth Oriented Space Science and Technology

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Spacecraft Technology 2 (SCT 2)

(ECTS: 4; SWS: 3)

Lecturers

Dr. Martin Rott, Univ.-Prof. Dr. Ulrich Walter
prerequisites   SCT 1
objectives  

Based on the foundations given in SCT I and upon completion of this course the student will be able to:

- understand the basics of mission design,
- carry out a simple satellite design,
- assess all essential subsystems of a satellite in terms of technology,
  environmental interaction and trade-off issues,
- be aware of the complex interactions of all subsystems of a satellite.
contents   The course shall provide knowledge of the fundamentals of space mission and spacecraft design:
Mission Design (requirements, trade studies); Mission Geometry & Orbit Selection; Orbit Perturbations; Space Environment; Satellite Payloads (typical); Structure & Mechanisms; Attitude Determination and Control System; Propulsion System; Communication System; Power System; Thermal Control System.
literature   Lecture Notes

Downloads

ESPACE_Mission_Design_final.pdf (4,0 MB)
Astrodynamics_handouts.pdf (3,3 MB)
Orbit_Geometry.pdf (6,6 MB)
Environment_engl.pdf (6,4 MB)
Thermal_Control.pdf (2,1 MB)
Power_engl.pdf (4,2 MB)
ADCS_engl.pdf (4,4 MB)
Tutorial 7 Slides (885 KB)
Tutorial 08 LEO Pertubations (52 KB)
Tutorial 9 Problem (52 KB)
Tutorial 10 Slides (3,8 MB)
Tutorial 10 Problem (67 KB)