QB50 - BeEagleSat Inner - Outer Design Details and ADCS Testing - Integration
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1 QB50 - BeEagleSat Inner - Outer Design Details and ADCS Testing - Integration E. Yakut 1, M. Suer 1, M.S. Uludag 2, E. Bas 2, S. Turkoglu 2, A.R. Aslan 2, A. Hacıoğlu 3, M. Çelebi 3, M. E. Aydemir 3, S. Basturk 3, A. Telli 4 and S. Gökçebağ 4 1 GUMUSH Aerospace & Defense Ltd., Istanbul, Turkey 2 Istanbul Technical University, Istanbul, Turkey 3 Air Force Academy, Istanbul, Turkey 4 Havelsan, Ankara, Turkey 7 th European CubeSat Symposium Liège, Belgium 9-11 September 2015 Erdinç Yakut, R&D Engineer E - m a i l : e r d i n g u m u s h. c o m. t r
2 Outline BeEagleSat Overview Design Requirements Subsystem Configuration Solar Panel Design Access Hatch and RBF ADCS Integration & Testing 2
3 BeEagleSat Overview Collaboration between Istanbul Technical University Turkish Air Force Academy GUMUSH Aerospace & Defense Ltd. Co. ErTek Space Tech. Ltd. Co. HAVELSAN Inc. Part of the QB50 project Design shall be fitted QB50 requirements. Multi Needle Langmuir Probe (mnlp) payload was selected. Second Payload X-Ray detector It is developed with collaboration between Sabanci & ITU. BeEagleSat ISO View 3
4 Payloads of BeEagleSat MULTI NEEDLE LANGMUIR PROBE (mnlp) X-RAY DETECTOR (XRD) For more information: For more information: 5th European CubeSat Symposium, The X-ray Detector on BeEagleSAT, E. Kalemci, A. Atasever, E. Umit and R. Aslan 4
5 Design Requirements mnlp have to be at RAM direction. -- QB50 XRD have to be at bottom or upper location. -- Second Payload Location of the CubeSat s CoG as far as possible ahead of the CoP in flight direction. QB50 ADCS The CubeSat CoG shall be located within a sphere of 20 mm from its geometric center. CDS Rev. 12 The moment of inertia about any satellite body axis for the host satellite on which the QB50 ADCS will be used shall not exceed 0.02 kgm2. -- QB50 ADCS The Y moment of inertia (Iyy) shall be at least 5% larger than the X and Z inertia moments (Ixx and Izz). Ref: QB50 System Requirements and Recommendations Issue 7 Y Z Ref: QB50 ADCS Interface Control Document Rev. 3 X 5
6 Design Requirements Each Solar panel has to have 4 solar cells(39.7 x 69.1 mm) or equivalent due to power requirement. ADCS has two lens & lens` location is fixed due to solar cell location. Access hatch shall to be at opposite ram direction. Remove Before Flight (RBF) tags should be able to be removed through these access hatches only. Likewise, Apply Before Flight (ABF) tags should only be accessible via these access hatches. ABF RBF Ram Direction 6
7 Subsystem Configuration mnlp Mechanism Card ADCS OBC-Beacon 20Whr Battery EPS UHF-VHF Modem Mechanism Card Control the antenna deployment system Edit CoG location and moment of inertias XRD 7
8 BeEagleSat View Ram Direction Zenith Direction Nadir Direction Deployed Configuration 8
9 Solar Panel Design Thermistor Area Monopole Antenna Holder Course Sun Sensor Antenna Deployment Swicth GPS Patch Antenna Panel 1 - Side Panel 1 Panel 2 Zenith Panel 9
10 Solar Panel Design Thermistor Area 50cm Monopole Antenna mnlp Deploment System Magnetometer Antenna Deployment Pin Panel 3 Side Panel 2 Panel 4 Nadir Panel 10
11 Access Hatch and RBF Kill Switch Termistor Area Apply Before Flight Pins Required Hole for XRD Cristal RBF Pin 11
12 ADCS Integration & Testing 12
13 ADCS Integration & Testing 13
14 ADCS Integration & Testing Sun Sensor testing: focused (left), unfocused (right) 14
15 ADCS Integration & Testing Nadir Sensor testing: focused (left), unfocused (right) 15
16 ADCS Integration & Testing Nadir Sensor (left), Sun (right) 16
17 ADCS Integration & Testing 17
18 ADCS Integration & Testing Temperature (C) Vacuum 25,00 NO 22,60 High 50,00 High 50,00 High 40,00 High 30,00 NO Nadir Sensor (left), Sun (right) 18
19 ADCS Integration & Testing Measured and controlled status are; Vacuum Temperature(C) Temperature of CPU Temperature of RateSense Enable Status Errors Sensors Power Consumption MCU Reaction Wheel Magnetorquer NO 25,00 NO 26,00 HIGH 22,60 24,00 30,00 HIGH 50,00 50,00 56,00 HIGH 50,00 50,00 58,00 HIGH 40,00 41,00 - HIGH 30,00 33,00 - NO 25,00 25,00 29,00 19
20 Thank you! Questions? Address: Web Site: 20
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