Unit information: Space Systems in 2012/13

Unit name	Space Systems
Unit code	AENG22300
Credit points	10
Level of study	I/5
Teaching block(s)	Teaching Block 2 (weeks 13 - 24)
Unit director
Open unit status	Not open
Pre-requisites	None
Co-requisites	None
School/department	School of Civil, Aerospace and Design Engineering
Faculty	Faculty of Engineering

Description including Unit Aims

The unit introduces spacecraft engineering and space based technology from a system level perspective. It introduces such fundamental topics as orbital mechanics, spacecraft subsystems (power, thermal, propulsion, communication, mechanisms and structures), with an emphasis on how these systems work together to deliver a specified objective. Payloads, launch systems and infrastructure are also considered, allowing the entire field of space applications to be appreciated.

Intended Learning Outcomes

On successful completion of the course students will:

• have a basic knowledge of all spacecraft subsystems;
• be able to perform simple calculations on Keplerian orbits, orbit transfers, propulsion systems, and some subsystem topics;
• be aware of the major technological applications, and how they are implemented in real missions;
• be able to place the knowledge of space systems engineering into the wider context.

Teaching Information

24, 50 minute lectures and 6 hours computing laboratory work, based around the Satellite Tool Kit package.

Assessment Information

Short answer assessed computing laboratory exercise, conducted in the 6 hours lab time (10%), 2 hr examination (1 compulsory short answer question, and 2 long from 4) in May/June (90%).

Reading and References

• Spacecraft Systems Engineering by Peter Fortescue and John Stark, 3rd edition Wiley
• Spacecraft Mission Analysis and Design by Wertz and Larson 3rd edition, Springer