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ENAS202
Syllabus
ENAS202
Introduction to CubeSats
Overview
Syllabus
Old questions
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