Master Thesis - OUFTI-1

More documents

Recommendations

Info

[53] J.-C. GOLINVAL. "Vibration Testing and Experimental Modal Analysis ". LTAS, University of Liège, Belgium, 2010. [54] D. STEINBERG. "Vibration Analysis for Electronic Equipments ". John WILEY & Sons, 2000. [55] "Deltatec Website". http://www.deltatec.be/ [56] "Samcef-Field Help". [57] J. PEDERSEN. "Vega CubeSats ICD, Issue 0, Revision 4 ". ESA-ESTEC, Noordwijk, The Netherlands, 2009. [58] J. BROWN. "Test Pod User's Guide Revision 6 ". California Polytechnic State University, San Luis Obispo, United States, 2006. [59] "ECSS-E-30 Part 2A - Space Engineering - Mechanical - Part 2: Structural ". ESA-ESTEC, Requirements & Standards Division, Noordwijk, The Netherlands, 2000. [60] G. ROETHLISBERGER. "SwissCube - Phase C: Launch Environment ". Lausanne, Switzerland, 2008. [61] P. GALEONE. "Approach for the Structural Tests for the Qualication of the CubeSats/P-PODs". ESA-ESTEC, Noordwijk, The Netherlands, 2009. [62] N. FRANCOIS. "ITR - Data Package: Subsystem STRU ". Technical Report, University of Liège, Belgium, 2010. 129
Appendix A Schemas of solar panels Figure 6.1: Schemas of solar panels +X and +/ − Y [15] 130
Page 1 and 2:
University of Liège Faculty of App
Page 3 and 4:
Abstract OUFTI-1, standing for "Orb
Page 5 and 6:
3.4 Initial idea . . . . . . . . .
Page 7 and 8:
List of Figures 1.1 The Pumpkin's C
Page 9 and 10:
4.18 MAC matrix using the simple me
Page 11 and 12:
List of Acronyms ADCS Al AlNiCo ASI
Page 13 and 14:
Thesis outline This thesis focuses
Page 15 and 16:
of larger satellites. So, the CubeS
Page 17 and 18:
1.2 OUFTI-1 project 1.2.1 Genesis O
Page 19 and 20:
• XatCobeo (Vigo - Spain): Develo
Page 21 and 22:
Chapter 2 OUFTI-1: Flight system co
Page 23 and 24:
Figure 2.2: Product tree of OUFTI-1
Page 25 and 26:
2.3.2 Solar panels The armor panels
Page 27 and 28:
• We do not want to drill or manu
Page 29 and 30:
In our case, because of the limited
Page 31 and 32:
Figure 2.13: Magnetic eld obtained
Page 33 and 34:
Figure 2.17: Pictures of the ADCS c
Page 35 and 36:
consider the possibility of oshorin
Page 37 and 38:
Figure 2.20: Exploded view of OUFTI
Page 39 and 40:
I xx , I yy and I zz are called the
Page 41 and 42:
Subsystem: Structure & Conguration
Page 43 and 44:
Subsystem: Thermal Control Parts Co
Page 45 and 46:
Chapter 3 Design of a new support f
Page 47 and 48:
Figure 3.3: Batteries during and af
Page 49 and 50:
The concept is the following one: F
Page 51 and 52:
A test under vacuum conditions was
Page 53 and 54:
Thermal Expansion (CTE) of the mate
Page 55 and 56:
Figure 3.9: Classication by density
Page 57 and 58:
The last property to determine is t
Page 59 and 60:
• So, it was decided to use two t
Page 61 and 62:
is to prevent the batteries' bulge.
Page 63 and 64:
• Then, the thermostats, that wil
Page 65 and 66:
Figure 3.23: Schematics of the cove
Page 67 and 68:
• Other components, including the
Page 69 and 70:
3.9.3 Dynamic behavior Finally, it
Page 71 and 72:
3.10 Summary Through this chapter,
Page 73 and 74:
Chapter 4 Electronic cards dynamic
Page 75 and 76:
Figure 4.1: Example of manufacturin
Page 77 and 78:
Figure 4.4: Illustration of the exp
Page 79 and 80: Figure 4.5: MAC between the two mod
Page 81 and 82: • Global mass/stiness smearing me
Page 83 and 84: 4.2.6 Modeling of the chassis A gen
Page 85 and 86: Q = ω k = 1 ω b − ω a 2 ζ ⇒
Page 87 and 88: Their study was based on the fact t
Page 89 and 90: Figure 4.14: Example of spacecraft
Page 91 and 92: Figure 4.15: Location of measuremen
Page 93 and 94: Figure 4.18: MAC matrix using the s
Page 95 and 96: 4.3.6 Application of the local mass
Page 97 and 98: ρ P C 104 connector = 10.12 × 10
Page 99 and 100: According to this particular shape,
Page 101 and 102: This is due to the fact that this c
Page 103 and 104: environment. Then, this model is ex
Page 105 and 106: 5.2.4 Antenna support For the anten
Page 107 and 108: Components Young's moduli (GP a) Po
Page 109 and 110: Components Young's moduli (GP a) Po
Page 111 and 112: 5.3 Static analysis As described in
Page 113 and 114: Figure 5.9: Illustration of the com
Page 115 and 116: Figure 5.11: Maximal Von Mises stre
Page 117 and 118: Figure 5.12: First mode of OUFTI-1
Page 119 and 120: Figure 5.15: Precise PSD of Vega [5
Page 121 and 122: Chapter 6 Conclusions This master t
Page 123 and 124: provided for each method used. We h
Page 125 and 126: last versions of the Verication Con
Page 127 and 128: [13] Ph. LEDENT. "Design and Implem
Page 129: [40] "Dejond - Aluminum Catalog ".
Page 133 and 134: Appendix B Schemas of electronic ca
Page 135 and 136: Appendix C Fixations of the endless
Page 137 and 138: Appendix D Datasheet of the battery
show all

Master Thesis - OUFTI-1

Create successful ePaper yourself

Delete template?

Save as template?