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Raketenantriebe 2 und Entwurfswettbewerb

ED110095Master's Modules5 ECTSEnglishsummer semesterLehrstuhl für Raumfahrtmobilität und -antriebe (Prof. Manfletti)
AI-edited module sheet. Based on the TUMonline module description, edited for readability.Original in TUMonline

What it is about

In this module you design rocket engines in teamwork and learn the most important physical relationships and design trade-offs. At the end you will be able to dimension a complete rocket propulsion system and configure the subsystems so that mission requirements are fulfilled.

What you will be able to do

  • Overall system design of a rocket propulsion system with specification of central performance parameters
  • Application of software tools for the design of rocket propulsion systems
  • Dimensioning of the main subsystems and components (propellant feed, combustion chamber including injection and cooling, ignition)
  • Discussion of technical influences of modern technologies and development of initial innovation ideas

What the module consists of

  • LectureConveying the module concept, system engineering basics, review of the main elements from Space Propulsion I, introduction of the design competition and analysis tools
  • ExerciseDeepening of specific topics, advising the project groups to support the design competition
  • Design Competition / Project WorkTeam work for the practical design of a rocket engine according to mission requirements; basis of the assessment

Teaching method

  • Media-supported interactive lecturesIntroduction to concepts, methods and the design competition
  • Exercise with supervised group workDetailed discussion of topics and advisory support for the project work
  • Independent group workConducting the design competition, producing the report and the presentation
No dates in the current semester yet
There are no course dates for this module this semester yet. They usually get added during the semester.
Show past dates

LectureRocket Propulsion II and Design Challenge

  • Thu09:00–10:3000.020, come together (9377.EG.020)
    11× · 23.04.–16.07.
    • 23.04.
    • 30.04.
    • 07.05.
    • 21.05.
    • 28.05.
    • 11.06.
    • 18.06.
    • 25.06.
    • 02.07.
    • 09.07.
    • 16.07.

ExerciseExercise Rocket Propulsion II and Design Challenge

  • Thu10:30–12:0000.012, Seminarraum (9377.EG.012)
    11× · 23.04.–16.07.
    • 23.04.
    • 30.04.
    • 07.05.
    • 21.05.
    • 28.05.
    • 11.06.
    • 18.06.
    • 25.06.
    • 02.07.
    • 09.07.
    • 16.07.

From an earlier semester, for reference only.

Show TUMonline data
Sprache
Englisch
Turnus
Sommersemester
Modulniveau
Master
Moduldauer
Einsemestrig
Gesamtstunden
150
Präsenzstunden
60
Eigenstudiumstunden
90
Organisationsname
Lehrstuhl für Raumfahrtmobilität und -antriebe (Prof. Manfletti)

Courses

  • Raketenantriebe 2 und Entwurfswettbewerb
  • Raketenantriebe 2 und Entwurfswettbewerb - Übung

Official page in TUMonline · Details are not binding.