ENAS202
Introduction to CubeSats
Syllabus
- Small Satellites and the Rise of a Standard (6 hours)
- Faster, better, cheaper
- 1990s satellite design and development
- Satellite in a Can: CanSat
- The CubeSat standard
- Amateur radio community
- Early years of CubeSat
- Current state of the standard
- CubeSat design essentials
- Satellite and space related developments in Nepal
- Current Nepali satellite/CubeSat projects
- CubeSat Design Process Overview (3 hours)
- From paper to space
- Lean satellite design philosophy
- Reverse satellite timeline philosophy
- CubeSat design reviews
- System block diagrams
- CubeSat safety review
- Frequency coordination with International Telecommunication Union (ITU)
- Satellite launch agreements
- Budgets, payments and financial considerations
- Procurement and logistics
- Space law and deorbit requirement considerations
- CubeSat Mission Design (9 hours)
- Mission statement and objectives
- Mission requirements
- Requirement allocation sheet (RAS)
- Mission success criteria
- CubeSat mission case studies
- State of art
- CubeSat systems-level state-of-art
- Constellation designs
- Formation flying
- Deep space missions
- Fly-by missions
- Deorbit missions
- CubeSat Hardware (12 hours)
- Commercial off-the-shelf (COTS) technologies
- The printed circuit board
- CubeSat bus standards
- On-board computer (OBC)
- Electrical power system (EPS)
- Solar panel designs (SP)
- Communication system (COM)
- CubeSat structure design (STR)
- CubeSat attitude determination and control system (ADCS)
- Thermal design considerations
- Deployables
- Design models and system redundancies
- Interface control document (ICD) and harnessing
- Manufacturing techniques and design for manufacturing (DFM)
- CubeSat integration facilities
- CubeSat Software (6 hours)
- Review of C programming language
- Integrated development environments (IDE)
- Free and open-source software (FOSW)
- Flight software (FSW)
- Fault detection, isolation and recovery (FDIR)
- CubeSat operating system (OS)
- CubeSat operational algorithms
- CubeSat simulations
- CubeSat Testing (6 hours)
- Triple T standard: test, test, test
- Space environment overview
- Popular CubeSat orbits
- The ISO 19683:2017 satellite testing standards
- Component screening
- Thermal vacuum testing (TVT) and thermal baking (TB)
- Vibration testing (VT)
- Radiation testing (RT)
- Anechoic chamber testing (ACT)
- Long duration tests (LDT) and long range tests (LRT)
- Qualification, proto-flight and acceptance testing
- Acoustics, spacecraft charging and other tests
- Testing platforms (flat-sats, electrical ground support equipment)
- Launch, Ground Segment and Operations (6 hours)
- CubeSat common launchers
- Communication frequencies, modulations
- IARU, API and ITU coordination
- Ground stations
- Antenna designs and considerations
- Ground sensor terminals
- Wireless communications link budget
- CubeSat failures
Evaluation
- Chapter 1 (6 hours): 10 marks
- Chapter 2 (3 hours): 5 marks
- Chapter 3 (9 hours): 10 marks
- Chapter 4 (12 hours): 15 marks
- Chapter 5 (6 hours): 10 marks
- Chapter 6 (9 hours): 10 marks