Mission Design for the CubeSat OUFTI-1
Mission Design for the CubeSat OUFTI-1
Mission Design for the CubeSat OUFTI-1
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CHAPTER 11.TESTSof asking <strong>for</strong> some notching as soon as <strong>the</strong> damping coefficients of our systemare experimentally known.A <strong>the</strong>rmal balance test will be per<strong>for</strong>med at <strong>the</strong> same time of <strong>the</strong> <strong>the</strong>rmalvacuum test. An acoustic test should not be carried out, because <strong>the</strong> facility<strong>for</strong>eseen <strong>for</strong> <strong>the</strong> test cannot per<strong>for</strong>m such a test and because <strong>the</strong> acoustic vibrationsneed to be considered only <strong>for</strong> huge surfaces.Be<strong>for</strong>e, during and after tests verifications will take place including dimensionalchecks, visual inspection and functional test.The University of Liège disposes of two important test facilities that will beused <strong>for</strong> <strong>OUFTI</strong>-1.Vibration and environment tests will be per<strong>for</strong>med at Liège Space Center (CSL),an university research center which is also an ESA-coordinated test facility. Inthis facility, satellites (like Planck) and space instruments are usually tested.Even more important in <strong>the</strong> present context, <strong>the</strong> <strong>CubeSat</strong> Compass-1 was alsotested with <strong>the</strong> cooperation of German and Belgian students, supervised byCSL staff.Electromagnetic compatibility test will be instead per<strong>for</strong>med at <strong>the</strong> ElectromagneticCompatibility Laboratory of <strong>the</strong> university. Since 2003, it is accreditedby <strong>the</strong> Belgian Organization <strong>for</strong> Accreditation (BELAC) under <strong>the</strong> ISO 17025norm.In principle, radiation tests are also possible at IPNAS, an university researchcenter, but <strong>the</strong>y will probably per<strong>for</strong>med only <strong>for</strong> some electronic equipment.11.2 Mechanical testsDuring launch, a satellite experiences an extremely hard dynamical environment.It is in fact stressed at all <strong>the</strong> frequencies depending on <strong>the</strong> missionphase:• Continuous accelerations due to launcher’s ascension. They don’t usuallygenerate problems and do not need to be tested.• Sinus vibrations at low frequency (f