Egyptian Space Science and Technology Educational Project Based on Can-Sat Program (CLTP)
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1 Egyptian Space Science and Technology Educational Project Based on Can-Sat Program (CLTP) Samy Amin, Hassan Ali, Omar Magdy, Mohammad Khalil Aerospace Engineering Department, Cairo University. EGYPT [CanSat Training Program - 1] Space System Technology Laboratory 1
2 Table Of Contents: 1- Egyptian CanSat Training Program (CTP-1) 2- Engineering the CanSat 3- Testing and Results 4- Conclusion 5- Achievements 6- Future plans 2
3 Egyptian CanSat Training Program (CTP-1) Number of trainees: 20 (Undergraduate /Aero. Students) Venue: Aerospace and Aeronautical department Number of teams: 3 Duration: 10 days 3
4 CTP-1 working phases Announcement [Posters & Facebook & mailing list] Orientation sessions Applications (CV s) Filtrations [Interviews] Selections Teams determination Hardware purchase Laboratory preparation [Tools & Internet & Catering] CTP-1 sessions Testing 4
5 5
6 Engineering of CanSat modules CanSat model 1- CanSat 3-Launcher (satellite) 2- Parachute 6
7 CanSat Mission Profile 7
8 1- CanSat CanSat architecture Gyroscope Accelerometer Temperature Pressure Wireless Communication Module GPS Mbed Microcontroller Serial Interface Camera Receiver On-Board Camera Module 8
9 MEMS (Hardware) 9
10 Coding, Testing and System Implementation 10
11 CanSat system integration and Fabrication Hard foam Shock absorbing 11
12 2- Parachute Parachute models : 1- Hemisphere 2- Para-sheet Gap + Spill hole Para-sheet Spill hole 12
13 Formulas and Tables Used in Parachute Design Equation of Area Vs. Velocity descend and Mass M :Mass of the CanSat G :Gravitational acceleration C d :Coefficient of drag estimated or verified by tests V :The velocity of decent, A :Designing area of the parachute Coefficient of drag estimated Spill hole design Non-linear relation 13
14 3- Launcher Launcher options: 1-Amature rockets 2-Balloon 3- RC planes 4- High Building 5-Water rocket ( ) 14
15 Water rocket compartment 15
16 Water rocket test (dummy payload) 16
17 Height [m] Water rocket specifications Volume: 2L pet bottle Pressure: 8 bars Altitude (Single bottle): m {experimentally} Fins: 3 on 120 o Faring: available Water Air %: (30% - 70%) Releasing mechanism: manual Deployment mechanism: Wireless Development: a)multi tanks b)multi boosters Problems: 1)Adhesives 2)Drag Time [sec.] Without payload With 300 g payload Simulator results for 50% water ratio a b 17
18 Phase 1 Phase 2 Phase 3 Testing and Results Testing Cycle Of CanSat Ground Test Data logging Drop Test Mission Profile (Free fall) Flight Test Water Rocket 18
19 Drop test (High building-ground camera) 19
20 Drop test (High building-on body camera) 20
21 CanSat Outcomes CANTASTIC 1 st MASRY 2 nd ENKSHARIAN 3 rd 21
22 CanSat axis demonstration Z X Y 22
23 Phase 1-Sample results of Ground test (altitude) in Aerospace Dept. 23
24 Phase 2-sample results of Drop test-1(altitude) of a 30m high building 24
25 Phase 2-sample results of Drop test-1 (acceleration) of a 30m High Building 25
26 Phase-3 sample results of Flight test (altitude) of a 12m launch of Water Rocket 26
27 Results conclusion Readings are very noisy due to many reasons Filtration of sensors readings is very important for control reasons We have two filtration approaches Hardware [Gyroscope] Software [Accelerometer] 27
28 Filtration: 1-Software Filter Difference between the ACCELEREATION before and after the filtration by same DROP Test profile 28
29 Filtration: 2-Hardware Filter Sample results of Drop test #2 Azimuth angle after hardware filtration 29
30 Achievements The Egyptian CanSat has won the prize of the Best Mechanical Engineering Project of the Egyptian Engineering Day [EED 10 th round], held byieee GOLD on the 9 th September Cairo University has established the very early version of the Space activity laboratory, the SPACE SYSTEM TECHNOLOGY LABORATORY [SSTL]. 30
31 Future Plans Prepare training program CTP-2 Egypt [7 weeks from now] Mission analysis and design [7 weeks from now] Participate in International competitions: ARLISS-2012 America. Mission Idea Contest 2012 Japan. Be a UNISEC-Egypt branch. National Competitions: Made In Egypt [MIE 2012] Prepare the first Egyptian CanSat competition. Scientific activities: Rover-back [On going] Mission oriented advanced CanSat [On going] BallonSat [1 year] CubeSat [3 years] 31
32 32
33 Thank you!! Questions?! 33
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