"Spazio. e Radioamatori " AMSAT Italia e C.I.S.A.R. Per il convegno. SpaceLab. organizzato da. Roma, 2 Dicembre 2006
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1 Per il convegno "Spazio e Radioamatori " organizzato da AMSAT Italia e C.I.S.A.R. Roma, 2 Dicembre 2006
2 The Institute Scuola Universitaria Professionale A practice-oriented, innovation-devoted higher education institution Delivers graduates ready to face the challenges of the real world In touch with enterprises
3 Where TIsat-1 - Lugano PICPOT PalaMede ALMASat ITAMSAT UNISAT and more IBo/PCe/AWe 3 / totale
4 So, WHY TIsat-1 The satellite is primarely an effective educational mean to create motivation, responsibility, novelty and enthusiasm IBo/PCe/AWe 4 / totale
5 Payload: our mantra For a university satellite the most important payload is not what you launch, but what safely remains on the ground: System design skills with focus on critical environment conditions high reliability do-it-right first interoperability of wide range of systems Teamwork attitude and skills Scientific networking with highly qualified partners From concept to product, students see the end-to-end process IBo/PCe/AWe 5 / totale
6 The Facets On Board Computer and subsystems Attitude Detection and Control TISat-1 Ground Segment Computer Simulations Mechanical Design Power Supply Communication IBo/PCe/AWe 6 / totale
7 Scuola Universitaria Professionale SI P SU Study Research Build Verify Launch Monitor IBo/PCe/AWe Running Activities 7 / totale
8 GS: HW/SW concept 80% done Private area Public area browser Internet browser Antenna and and Radio System Tracking System HTTP Web Interface browser IBo/PCe/AWe 8 / totale
9 Antenna - Radio System Present Version TCP/IP Connection Internet YAESU G-5500 Rotors and Az/El Controller TCP/IP Connection Radio transceiver YAESU FT-8800E Radio receiver YAESU VR-5000 RS Analog audio RS-232 Analog audio Future Version Radio Link DSP Data Decoding IBo/PCe/AWe 9 / totale
10 Tracking System 100% done To Remote Antenna and Radio System Internet Tracking System Web Interface Satellite Position Predictor Position Data Satellite Data Database Satellite visualization Satellite selection IBo/PCe/AWe 10 / totale
11 Web Interface 100% done Ground Station Satellite Tracking Internet Public area Satellite Visualization Homepage Private area Login Database Satellite Selection IBo/PCe/AWe 11 / totale
12 Mockups and Experiments Pulsed Plasma Thruster Levitron and Magnetorquer Levitron (2kg lift) with Momentum Wheel Experiment IBo/PCe/AWe 12 / totale
13 Thermal Test in Vacuum IBo/PCe/AWe 13 / totale
14 For a 700km, circular, polar orbit, 1 to 6 months mission Many points still open Temperatures on and in the spacecraft: reliable data? Batteries: temperature issues? Electronic COTS: bipolar vs. MOS devices for radiation tolerance? Attitude: materials for passive control and damping? Composite structures for space: caveats? Rock-solid beacon: HowTo? Antennas: a mechanical issue, more than a radiation one? An alternative path to the launcher? (actually Cal-Poly) IBo/PCe/AWe 14 / totale
15 Contact Welcome to IBo/PCe/AWe 15 / totale
16 Knowledgeable Partners Welcome In Space in partnership with YOU Thank you AMSAT-I IBo/PCe/AWe 16 / totale
17 Staff 2006 P. Ceppi, ing. el. dipl. ETHZ; docente DTI A. Graf, dipl. fisico ETHZ; docente DTI G. Salvadè, dipl. fisico ETHZ; docente DTI A. Weston, ing. el. dipl. ETHZ; docente DTI I. Bonesana, ing. inf. S. Puseljic, ing. el. A. Spiga, ing. inf. P. Speranza, tec. el. L. Tognetti, tec. el IBo/PCe/AWe 17 / totale
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