The 2007 CubeSat Developers' Workshop SwissCube Project
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1 SwissCube Project ( The 2007 CubeSat Developers' Workshop SwissCube Project Guillaume Roethlisberger Mechanical System Engineer Space Center EPFL Fabien Jordan Electrical System Engineer Space Center EPFL Prof. Herbert Shea EPFL Microsystems for Space Technologies Laboratory Dr. Maurice Borgeaud Director, Space Center EPFL Muriel Noca Project Manager Space Center EPFL Guillaume Roethlisberger & Fabien Jordan 19 April 2007
2 SwissCube Project Goal: to have a Swiss cubesat in orbit by end of 2008 Satellite and ground segment defined, designed, built, tested and operated by students. Multi-disciplinary, multi-lab, multi-university collaboration Strong educational aspect: student/industry ties, ESA/NASA development phases and standards SwissCube Ground Stations Budget ~ 400 kusd (including launch), over 3 years already gathered 2/3 of budget 2
3 Mission Objectives Objective 1 Deliver a fully tested cubesat to launch site Photo NASA Objective 2 Launch, close RF link and download telemetry Objective 3 Receive Science data and characterize operations Science Objective Characterize variability of Airglow phenomena in intensity and altitude Fly a new SPAD for use as a technology demonstration for the development of a lowcost Earth sensor 3
4 Mission Characteristics Launch DNEPR or/and VEGA launch vehicle Orbit Sun-synchronous Inclination ~ Orbital altitude ~ km Orbital period ~ min Eclipses ~ 30 % of orbital period Avg. power ~ 1.8 W (Power bus voltage: 3.3 V) Mean pass duration ~ 10 min Data downlink rate ~ 1 kbps 4
5 System Overview The 2007 CubeSat Developers' Workshop Lithium- Polymer technology Hardware and software beacon generator No Connector Wires are welded Permanent magnet Determination MSP430 MSP430 MSP430 EPS Full Redundancy Antennas (2 monopoles) 32 bit ARM Processor MSP430 5
6 System Overview The 2007 CubeSat Developers' Workshop Electrical Power System Current Control Current Control Current Control 6
7 System Overview Structure & Configuration Structure Monobloc concept => Mass: 106 grams Machined per CNC and electro-errosion 7
8 System Overview Structure & Configuration Configuration Two principal constraints: Payload PCBs 8
9 Test Plan - Model Philosophy Phase C Structural and Thermal Model (STM) Dummies Integration Model (IM) Functionally representative in terms of electrical and software 9
10 Test Plan - Model Philosophy Phase D Engineering Qualification Model (EQM) Flight representative, tests at qualification level 2 Flight Models (FM) Tests at acceptance level 10
11 Conclusion Next important deadlines : CDR - Nov 07 / QR April 08 / AR August 08 2 launches - Nov+Dec 08 Critical items: Permanent magnets Control algorithm Composites and adhesive bonding Solar Cells bonding Tests in general (radiation, EMC) All advices, sharing of experience are welcome, and remunerated by Swiss chocolates! For more details or contact : fabien.jordan@epfl.ch guillaume.roethlisberger@epfl.ch 11
12 Celebrating Sputnik 50th Anniversary October 4, 2007 Lausanne, Switzerland 3 rd EPFL Space Research Day Early days of the space conquest and visions for the future What was is like to build a small satellite then? What is it like now? 12 More info : muriel.noca@epfl.ch
13 Questions? The 2007 CubeSat Developers' Workshop Thank you for your attention!!! 13
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