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Project M.E.T.E.O.R.

Project M.E.T.E.O.R. P07109: Flying Rocket Team Andrew Scarlata, Geoff Cassell, Zack Mott, Garett Pickett, Brian Whitbeck, Luke Cadin, David Hall. Inner and Outer Shell ANSYS Stress Modeling ( Chalice Design). Payload. Composite-Honeycomb End Cap. Electronics. Micro IMU

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Project M.E.T.E.O.R.

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  1. Project M.E.T.E.O.R. P07109: Flying Rocket Team Andrew Scarlata, Geoff Cassell, Zack Mott, Garett Pickett, Brian Whitbeck, Luke Cadin, David Hall

  2. Inner and Outer Shell ANSYS Stress Modeling(Chalice Design) Payload Composite-Honeycomb End Cap Electronics Micro IMU (Inertial Measurement Unit) Composite Outer Shell Nitrous Oxide Tank Pre-Combustion Chamber HTPB Fuel Grain Post-Combustion Chamber Graphite Nozzle

  3. Inner and Outer Shell ANSYS Stress Modeling(Embedded Design) 2x Aluminum End Cap Siphon Tube Composite Outer Shell (Aluminum Inner Reinforced) Nitrous Oxide Tank Titanium Inner Shell Combustion Chamber Inside 2x Outer Ring

  4. Customer Specifications

  5. Bill of Materials

  6. Mass Budget

  7. Composite Pressure Vessel(Chalice Concept) Nitrous Oxide Vapor Liquid Nitrous Oxide • Identified Company (CompositeX) to manufacture Custom Composite Pressure Vessel • Working pressure 1000psi • Holds 8 kg Nitrous Oxide • 700 cubic inch volume • HDPE lined • 1.4 lbs

  8. Composite Pressure Vessel(Chalice Concept) Helium Gas Liquid Nitrous Oxide

  9. Composite Pressure Vessel(Chalice Concept) • Ideal gas law used to model helium pressure • p=m*R*T/V • Verified from pressure/ temperature data that Helium will remain gaseous • Compressibility factor ~1, so ideal gas assumption valid • Tank weights listed estimated from quote of 700ci=1.4 lbs • Also includes weight of Helium (case dependent)

  10. Aluminum/Titanium Comparison

  11. Mass Calculation

  12. Mass CalculationChalice Design, 7075-T6 Al240mm OD, 1.75mm Thickness, FS 1.25

  13. Mass CalculationEmbedded Outer Shell Design, 7075-T6 Al 180mm OD, 61mm ID, 1.3mm Thickness, FS 1.25

  14. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Model Geometry Inner Shell (fuel grain housing) Outer radius: 2.40” (~61mm) Inner radius: 2.36” (~60mm) Height: 21.46” (~545 m) Mat’l: Aluminum 7075 T6 Outer Shell (NOS/rocket housing) Outer radius: 1.75” + 0.5 mm (0.03225 m) Inner radius: 1.25” (0.03175 m) Height: 1.5” (0.0381 m) Mat’l: Al 7075 T6 with Composite over-wrap Composite: IM7 Carbon (fiber) / PEEK (matrix)

  15. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Material Properties Carbon/PEEK Composite (Modeled as Orthotropic) Density: 1600 kg/m3 Longitudinal Mod., E1: 71.7e9 Pa Transverse Mod., E2: 10.2e9 Pa Poisson’s Ratio, v12: 0.30 Shear Modulus, G12: 5.7e9 Al 7075-T6 (Modeled as Isotropic) Density: 2810 kg/m3 Longitudinal Mod., E1: 71.7e9 Pa Poisson’s Ratio, v12: 0.33 PEEK (matrix) Density: 1376 kg/m3 IM7 Carbon Fiber (12,000 filaments) (Modeled as Orthotropic) Density: 1780 kg/m3 Longitudinal Mod., E1: 278e9 Pa Poisson’s Ratio, v12: 0.20

  16. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Outer Shell (w/ composite) Figure 1: Outer Shell of Imbedded Fuel Grain Design (Meshed Elements – 8node93)

  17. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Outer Shell (w/ composite) Figure 2: Outer Shell of Imbedded Fuel Grain Design: Plot Results  Contour Plot  Element Solution  Stresses  von Mises stress

  18. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Outer Shell (w/ composite) Figure 3: Outer Shell of Imbedded Fuel Grain Design: Plot Results  Deformed Shape  Def + undeformed

  19. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Outer Shell (w/ composite) Figure 4: Outer Shell of Imbedded Fuel Grain Design: (Pressure & Constraints – Rotated view)

  20. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Outer Shell (w/ composite) Figure 5: Outer Shell of Imbedded Fuel Grain Design: (Pressure & Constraints - Front View)

  21. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Outer Shell (w/ composite) Figure 6: Outer Shell of Imbedded Fuel Grain Design: (Pressure & Constraints - Side View)

  22. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Inner Shell (All Aluminum) Figure 7: Inner Shell of Imbedded Fuel Grain Design (Meshed Elements – 8node93)

  23. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Inner Shell (All Aluminum) Figure 8: Inner Shell of Imbedded Fuel Grain Design: Plot Results  Contour Plot  Element Solution  Stresses  von Mises stress

  24. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Inner Shell (All Aluminum) Figure 9: Inner Shell of Imbedded Fuel Grain Design: Plot Results  Deformed Shape  Def + undeformed

  25. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Inner Shell (All Aluminum) Figure 10: Inner Shell of Imbedded Fuel Grain Design: (Pressure & Constraints – Rotated view)

  26. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Inner Shell (All Aluminum) Figure 11: Inner Shell of Imbedded Fuel Grain Design: (Pressure & Constraints – Front view)

  27. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Inner Shell (All Aluminum) Figure 12: Inner Shell of Imbedded Fuel Grain Design: (Pressure & Constraints – Side view)

  28. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Outer Shell (Aluminum only) Figure 13: Outer Shell of Imbedded Fuel Grain Design (Meshed Elements – 8node93)

  29. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Outer Shell (Aluminum only) Figure 14: Outer Shell of Imbedded Fuel Grain Design: Plot Results  Contour Plot  Element Solution  Stresses  von Mises stress

  30. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Outer Shell (Aluminum only) Figure 15: Outer Shell of Imbedded Fuel Grain Design: Plot Results  Deformed Shape  Def + undeformed

  31. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Outer Shell (Aluminum only) Figure 16: Outer Shell of Imbedded Fuel Grain Design: (Pressure & Constraints – Rotated view)

  32. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Outer Shell (Aluminum only) Figure 17: Outer Shell of Imbedded Fuel Grain Design: (Pressure & Constraints - Front View)

  33. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Outer Shell (Aluminum only) Figure 18: Outer Shell of Imbedded Fuel Grain Design: (Pressure & Constraints - Side View)

  34. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Figure 19: ELEMENT LAYERS

  35. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Figure 20: LAYER ORIENTATION AND THICKNESS

  36. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Figure 21: LAYER ORIENTATION AND THICKNESS continued…

  37. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Figure 22: COMPOSITE PROPERTIES

  38. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Figure 23: ALUMINUM PROPERTIES

  39. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Figure 24: FAILURE CRITERIA FOR COMPOSITES

  40. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Figure 25: INVERSE TSAI-WU STRENGTH RATIO INDEX

  41. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Figure 26: X-COMP OF STRESS

  42. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Figure 27: Y-COMP OF STRESS

  43. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Figure 28: X-COMP OF STRESS

  44. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Figure 29: SHEAR XY-DIR

  45. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Figure 30: SHEAR YZ-DIR

  46. Inner and Outer Shell ANSYS Stress Modeling(Embedded Fuel Grain Concept) Figure 31: SHEAR XZ-DIR

  47. Top and Bottom Fixture Solidworks Stress Model(Embedded Fuel Grain Concept) Model Geometry Mass = 0.520526 kg % Allowable Mass(2.31kg) = 22.5% Volume = 0.00018 m3 Geometry is the same for both the top and bottom fixture

  48. Top and Bottom Fixture Solidworks Stress Model(Embedded Fuel Grain Concept) 1000 psi 1000 psi Material Properties, Loading, and Meshing Al 7075-T6 Density: 2810 kg/m3 Modulus of Elasticity: 71.7 GPa Shear Modulus: 28 GPa Meshing done with Solidworks and Cosmos finite element analysis Elements: 25306 Nodes: 49277

  49. Top and Bottom Fixture Solidworks Stress Model(Embedded Fuel Grain Concept) Factor of Safety Results

  50. External Shell Solidworks Stress Model(Embedded Fuel Grain Concept) Model Geometry Mass = 1.63918 kg % Allowable Mass(2.31kg) = 71.0% Volume = 0.00058 m3

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