Moses - Space System Design Project

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Diese Modulbeschreibung gilt nicht im aktuellen Semester.

Die Modulbeschreibung gilt nur für den Zeitraum SoSe 2020 - WiSe 2020/21. Die Version für das aktuelle Semester (SoSe 2024) finden Sie hier: Modulbeschreibung des SoSe 2024

Module / Version:
#50040 / #1

Validity:
SoSe 2020 - WiSe 2020/21

Default display language:
English

Module title:
Space System Design Project

Credits:
9

Responsible person:
Ohe, Martin

Grading:
benotet

Type of exam:
Portfolioprüfung

Zugehörigkeit

Faculty:
Fakultät V

Institute:
Institut für Luft- und Raumfahrt

Area of expertise:
35341200 FG Raumfahrttechnik

Prüfungsausschuss:
Verkehrswesen

Kontakt

Office:
F 6

Contact person:
Ortega, Manuel

E-mail address:
Manuel.ortega@mse.tu-berlin.de

Website:

http://www.mse.tu-berlin.de

Learning Outcomes

The module imparts the basics of methodical approaches of spacecraft design for all segments of a space mission. A focus is set on design steps for spacecraft subsystems. The students shall be able to design any subsystem of a spacecraft to a certain degree. Methods of system verification, fault tolerant design and cost estimation shall be part of the basic knowledge of a prospective space systems engineer. Another focus in this course is to gain experience in working within an interdisciplinary group. Discussion and definition of interfaces, making compromises in trade-offs and focusing on a common goal in a team are daily routine in spacecraft engineering.

Content

- Spacecraft system planning - Space environment and considerations on designing a spacecraft - System integration - System verification - Space mission cost estimation - Space law - Phases and life cycle of a space project - Design reviews - Space project documentation

Module Components

Pflichtgruppe:

All Courses are mandatory.

Course Name	Type	Number	Cycle	Language	SWS	VZ
Space System Design Project	VL		WiSe	No information	4

Workload and Credit Points

Space System Design Project (VL):

Workload description	Multiplier	Hours	Total
Attendance	15.0	4.0h	60.0h
Self-study of lecture materials	15.0	14.0h	210.0h
			270.0h(~9 LP)

The Workload of the module sums up to 270.0 Hours. Therefore the module contains 9 Credits.

Description of Teaching and Learning Methods

Theoretical lectures and project work

Requirements for participation and examination

Desirable prerequisites for participation in the courses:

- Basics about space technologies - Basics about satellite technologies

Mandatory requirements for the module test application:

This module has no requirements.

Module completion

Grading

graded

Type of exam

Portfolio examination

Type of portfolio examination

100 Punkte insgesamt

Language

English

Test elements

Name	Points	Categorie	Duration/Extent
Final presentation	30	flexible	15 min
Midterm presentation	20	flexible	15 min
Project documentation	25	flexible	40 h
Quiz	25	written	30 min

Grading scale

Notenschlüssel »Notenschlüssel 2: Fak IV (2)«

Gesamtpunktzahl	1.0	1.3	1.7	2.0	2.3	2.7	3.0	3.3	3.7	4.0
100.0pt	95.0pt	90.0pt	85.0pt	80.0pt	75.0pt	70.0pt	65.0pt	60.0pt	55.0pt	50.0pt

Test description (Module completion)

A quiz covers questions related to the theoretical content of the lecture course. The project status shall be presented in a midterm and a final presentation. The project work shall be documented.

Duration of the Module

The following number of semesters is estimated for taking and completing the module:
1 Semester.

This module may be commenced in the following semesters:
Wintersemester.

Maximum Number of Participants

This module is not limited to a number of students.

Registration Procedures

Registration at the MSE secretary according to the MSE study and examination regulations. Dates and deadlines will be announced by semester start.

Recommended literature
Elements of Spacecraft Design, C.D. Brown, AIAA, 2002
Handbuch der Raumfahrttechnik, Hallmann, W. und Ley, W., München, Wien, Hanser 1999, 792 S.
Raumfahrtsysteme : eine Einführung mit Übungen und Lösungen, E. Messerschmidt ; S. Fasoulas. - Berlin u.a.: Springer, 2000. 533 S.
Spacecraft Structure and Mechanisms, T.P. Sarafin, Kluwer, 1995
Space Mission Analysis and Design, W. Larson, J. Wertz, Kluwer, 1999
Space Vehicle Mechanisms, P.Conley, New York, 1998

Assigned Degree Programs

Semester:

Zeige auch ausgelaufene Studiengänge und StuPOs

This module is used in the following Degree Programs (new System):

	Studiengang / StuPO	StuPOs	Verwendungen	Erste Verwendung	Letzte Verwendung
This module is not used in any degree program.

Miscellaneous

No information

Space System Design Project