MECH ENG 7073 - Space Vehicle Design
North Terrace Campus - Semester 2 - 2018
General Course Information
Course Code MECH ENG 7073 Course Space Vehicle Design Coordinating Unit School of Mechanical Engineering Term Semester 2 Level Postgraduate Coursework Location/s North Terrace Campus Units 3 Contact Up to 4.5 hours per week Available for Study Abroad and Exchange Y Incompatible MECH ENG 3025 or MECH ENG 4015 or MECH ENG 3104 Course Description The aim of the course is to introduce the students to the basic theories and design criteria of space vehicles. Historical developments in space flight are explained as are the basic rocket equations, as well as the principles of rocket staging and its optimisation. The course includes orbital and trajectory theory, where two-body motion, manoeuvres and special trajectories are described. Numerical integration will be introduced. Individual subsystems are covered in detail. A section about rocket propulsion focuses on performance, propulsion requirements and various propellant systems (monopropellant, bipropellant, solid, cold gas and electrical and electromagnetic propulsion systems). Also covered are environmental control and life support systems, electrical power subsystems, communications and thermal control systems. Matlab will be used throughout the course.
Course Coordinator: Dr Farzin GhanadiDr Farzin Ghanadi: email@example.com, Room S324h, extension 32293.
The full timetable of all activities for this course can be accessed from Course Planner.
Course Learning OutcomesOn successful completion of this course students will be able to:
1 Introduce students to Space Vehicle Design, its complex issues requiring expertise from many different areas of Aerospace Engineering; 2 Familiarise students with space vehicle types and subsystems; 3 Provide students with an understanding of the parameters that influence the design of space vehicles including their mission, orbital mechanics and the space environment; and 4 Equip students with analytical and numerical methods required to solve space vehicle design problems.
The above course learning outcomes are aligned with the Engineers Australia Stage 1 Competency Standard for the Professional Engineer.
The course is designed to develop the following Elements of Competency: 1.1 1.2 1.3 1.4 1.5 1.6 2.1 2.2 2.3 2.4 3.2 3.3 3.5 3.6
University Graduate Attributes
This course will provide students with an opportunity to develop the Graduate Attribute(s) specified below:
University Graduate Attribute Course Learning Outcome(s) Deep discipline knowledge
- informed and infused by cutting edge research, scaffolded throughout their program of studies
- acquired from personal interaction with research active educators, from year 1
- accredited or validated against national or international standards (for relevant programs)
1, 3 Critical thinking and problem solving
- steeped in research methods and rigor
- based on empirical evidence and the scientific approach to knowledge development
- demonstrated through appropriate and relevant assessment
1-3 Teamwork and communication skills
- developed from, with, and via the SGDE
- honed through assessment and practice throughout the program of studies
- encouraged and valued in all aspects of learning
2, 3 Career and leadership readiness
- technology savvy
- professional and, where relevant, fully accredited
- forward thinking and well informed
- tested and validated by work based experiences
2, 3 Self-awareness and emotional intelligence
- a capacity for self-reflection and a willingness to engage in self-appraisal
- open to objective and constructive feedback from supervisors and peers
- able to negotiate difficult social situations, defuse conflict and engage positively in purposeful debate
1, 2, 4
- Course notes
- Textbook: Peter Fortescue, Graham Swinerd, and John Stark, Spacecraft Systems Engineering, 4th Ed., Wiley, 2011,
- Any online material will be available at: https://www.adelaide.edu.au/myuni/
- Digital recordings of lectures (e.g., taping lectures, wireless network, pod-casts) may not be made available to students who are absent.
- Spacecraft Structures and Mechanisms – From Concept to Launch, 1995, Thomas Sarafin and Wiley Larson (editors).
- Spacecraft Mission Design, 1998, Charles D. Brown.
- Dynamics of Atmospheric Reentry, 1993, F.J. Regan and S.M. Anandakrishnan.
- Keys to Space, 2003, A. Houston and M. Rycroft.
Copies of assignments and any paper material distributed during class will also be posted on My-Uni.
Learning & Teaching Activities
Learning & Teaching Modes
Lectures supported by problem-solving tutorials and a practical laboratory developing material covered in lectures
The information below is provided as a guide to assist students in engaging appropriately with the course requirements.
A three unit course has a minimum workload of 156 hours regardless of the length of the course. It is expected that students spend 48hrs/week during teaching periods, additional time may need to be spent acquiring assumed knowledge, working on assessment during non-teaching periods, and preparing for and attending examinations.
Formal Contact: Lectures and tutorials: 45 hours,
Practical: 1.5 hours, Exam: 3 hours
Suggested personal workload (will vary between students): Reading and revising course material: 30-50 hours, Completion of assignments and practical report: 30-50 hours, Exam preparation: 30-50 hours.
Learning Activities SummaryThe numbers quoted here are approximations and will vary if some activities take more or less time than anticipated:
I. Introduction of Spacecraft – 4 Lectures
• Type of spacecraft
• Design procedure
• Spacecraft configuration
• System integration
II. Orbital mechanics – 7 lectures
• Basic of dynamics/orbital mechanics
• Types of trajectories
• Orbit transfers
• Geostationary Earth Orbits (GEO)
• Interplanetary missions
III. Propulsion system – 7 lectures
• Basic of aerodynamics and thermodynamics
• Chemical rockets
• Spacecraft propulsion
• Electric propulsion
• Advanced propulsion
IV. Launch systems – 4 lectures
• Rocket equation
• Rocket staging
• Basic launch vehicle performance and operations
• Spacecraft launch phases and mission planning
V. Planetary entry/re-entry – 4 lectures
• Fundamentals of hypersonic aerothermodynamics
• Ballistic re-entry
• Entry/re-entry issues
VI. Attitude control system – 4 lectures
• ACS overview
• Torques and Torquers
• Attitude measurement
VII. Electrical power system – 1 lecture
• Power system element
• Primary power source
• Secondary power source
VIII. Thermal control system – 2 lectures
• Fundamental of Thermal analysis
• Thermal design
• Thermal protection system
IX. Communication subsystem – 2 lectures
X. Space environment – 2 lectures
XI. Assembly, integration and verification – 2 lectures
XII. Student Seminars/Presentations – 4 lectures
XIII. Review of course material – 2 lectures
Specific Course Requirements
Students will be required to adhere to laboratory conduct safety guidelines for the practical component of this course.
The University's policy on Assessment for Coursework Programs is based on the following four principles:
- Assessment must encourage and reinforce learning.
- Assessment must enable robust and fair judgements about student performance.
- Assessment must maintain academic standards.
Assessment SummaryAll assessment is summative.
- Final Exam: 50%
- 5 Individual Assignments: 25%
- Group Assignment/Project: 15%
- Laboratory (Microgravity): 10%
Assessment task Weighting % Description Due date Learning objectives Assignment 1 5 Written individual assignment covering class material 1PM Monday week 3 1-4 Assignment 2 5 Written individual assignment covering class material 1PM Monday week 5 1-4 Assignment 3 5 Written individual assignment covering class material 1PM Monday week 7 1-4 Assignment 4 5 Written individual assignment covering class material 1PM Monday week 9 1-4 Assignment 5 5 Written individual assignment covering class material 1PM Monday week 11 1-4 Group Assignment/Project 15 Oral and written group assignment of designing your own spacecraft Monday Week 12 1-4 Laboratory 10 Microgravity 2 weeks after lab class or as specified by demonstrator 2, 4 Final Exam 50 Open-book exam covering all material covered in course Exam period 1-4
While every effort has been made to ensure that this information reflects an accurate plan, the coordinator reserves the right to make changes that ensure the continual improvement of the course. Any such changes will be communicated both during lectures and via MyUni.
Assessment Related Requirements
In order to pass this course, students must achieve a pass grade for the microgravity performance laboratory.
Final exam is a 3-hour long open book exam, to be conducted during the formal university examination period.
There will be 5 assignments in total. These are individual assignments (no collaboration). These will be distributed during class and also placed on MyUni. Due dates for these assignments may be subject to change; any changes will be announced in-class, written on the assignment, and posted on MyUni at the time the assignment is first distributed.
The microgravity laboratory is run as part of the formal Level III laboratories.
Unless otherwise specified, submission of assignments and laboratory reports will be made through the hand-in boxes located on Level 2 of Engineering South. Cover-sheets should be attached to all submissions (cover-sheets located next to the submission boxes).
Late submissions will be penalised at 20% per day late. All submissions are due at 1pm. Extensions for assignments will only be given in exceptional circumstances and a case for this with supporting documentation must be made either in writing after a lecture, submitted in hard copy to the front office (to be passed on to the lecturer), or emailed to the lecturer directly.
Assignments will be assessed and returned within 4 weeks from submission (usually significantly less). Assignments that are marked prior to the last class will be brought to class for students to collect. Any assignments not collected in-class will be left in the assignment collection boxes next to the elevator on level 2 of Engineering South. There will be no opportunities for re-submission of work of unacceptable standard. Due to the large class size, feedback on assignments will be limited to in-class discussion resulting from questions from students.
Grades for your performance in this course will be awarded in accordance with the following scheme:
M10 (Coursework Mark Scheme) Grade Mark Description FNS Fail No Submission F 1-49 Fail P 50-64 Pass C 65-74 Credit D 75-84 Distinction HD 85-100 High Distinction CN Continuing NFE No Formal Examination RP Result Pending
Further details of the grades/results can be obtained from Examinations.
Grade Descriptors are available which provide a general guide to the standard of work that is expected at each grade level. More information at Assessment for Coursework Programs.
Final results for this course will be made available through Access Adelaide.
The University places a high priority on approaches to learning and teaching that enhance the student experience. Feedback is sought from students in a variety of ways including on-going engagement with staff, the use of online discussion boards and the use of Student Experience of Learning and Teaching (SELT) surveys as well as GOS surveys and Program reviews.
SELTs are an important source of information to inform individual teaching practice, decisions about teaching duties, and course and program curriculum design. They enable the University to assess how effectively its learning environments and teaching practices facilitate student engagement and learning outcomes. Under the current SELT Policy (http://www.adelaide.edu.au/policies/101/) course SELTs are mandated and must be conducted at the conclusion of each term/semester/trimester for every course offering. Feedback on issues raised through course SELT surveys is made available to enrolled students through various resources (e.g. MyUni). In addition aggregated course SELT data is available.
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