Morning Session 1
1. Optical Design for Near Equatorial Satellite.
1.1 Theory
1.2 Spreadsheet Based Case Study
Short Break
Morning Session 2
2. Power Budget for Near Equatorial Satellite.
2.1 Theory and Calculation
2.2 Spreadsheet Based Case Study
Afternoon Session 3
3. Launch opportunity for piggyback (cubesat) satellite to Near Equatorial Orbit (NEqO) and Introduction to Orbital Simulation
3.1 Consideration for launch into NEqO (LV, SPASS, PPOD)
3.2 Introduction to Orbital Simulation
SHORT COURSE SCHEDULE
|
Date |
Time |
Event |
Venue |
|
11 July 2011 Monday |
8:00 am – 8:30 am |
Registration |
Board Room Foyer Level 2 |
|
8:30 am – 10:30 am |
Module 1: Optical Payload Design for Near Equatorial Orbit Hafizah Mohd Nasir, ATSB® |
Board Room Level 2 |
|
|
10:30 am – 11: 00 am |
Tea Break |
Board Room Foyer Level 2 |
|
|
11:00 am – 1:00 pm |
Module 2: Power Budget for Near Equatorial Satellite Mohd Amir Iskandar Mazlan, ATSB® |
Board Room Level 2 |
|
|
1:00 pm – 2:00 pm |
Lunch |
Coffee House Level 1 |
|
|
2:00 pm – 4:00 pm |
Module 3 Part 1: Launch Opportunity for Piggyback Satellites Mohd Faizal Jamaludin Wong, ATSB® |
Board Room Level 2 |
|
|
4:00 pm – 4:30 pm |
Tea Break |
Board Room Foyer Level 2 |
|
|
4:30 pm– 6:00 pm |
Module 3 Part II: Introduction to Orbital Simulation Mohd Nazree Dol Bahar, ATSB® |
Board Room Level 2 |
