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Roberto Gonzalez Sage Pasternacki Amanda Crawford Web Developer & Recorder, Primary Author, Project Manager & Secondary Editor & Document Manager Client Contact Garrett Wright Christian Johnson Primary Editor & Budget


  1. Roberto Gonzalez Sage Pasternacki Amanda Crawford Web Developer & Recorder, Primary Author, Project Manager & Secondary Editor & Document Manager Client Contact Garrett Wright Christian Johnson Primary Editor & Budget Liaison & Co-Solidworks Modeler Co-Solidworks Modeler October 24, 2016 Orbital ATK Team A

  2. PROJECT DESCRIPTION Orbital ATK has commissioned this capstone team to design a low-shock payload separation system that can be built in-house at a fraction of the cost compared to what is currently on the market by their competitors. (1) Work with Orbital ATK mechanical engineers to understand the needs and desires of the delivered project. (2) Survey commercially available separation systems. (3) Develop design concepts that meet all requirements. (4) Perform trade studies to down select to a single design. (5) Manufacture a prototype. (6) Provide Orbital ATK with PDR and CDR presentations. (7) Final product will include design, analysis and manufactured prototype. October 24, 2016 Garrett Wright Orbital ATK Team A

  3. FUNCTIONAL DECOMPOSITION October 24, 2016 Christian Johnson Orbital ATK Team A

  4. REQUIREMENTS Customer Requirements Engineering Requirements Target/Tolerance Low shock Can be stored and functional for up to 90 days 90 days Low relative cost Temperature range -10/75 C In-house manufacturability Immune to environmental conditions <90% humidity Compatible with existing payload systems Success rate 100% Withstand stresses during flight Withstand bending load 28,085 in-lbf Electrical pulse to signal separation Withstand shear loads 1,630 lbf Withstand axial loads 2,315 lbf Variable separation force 4.5-18 ft-lbf Tipoff angle <1 degree/sec Existing system compatibility 15 in. diameter with 24 ¼ in fasteners Factor of safety N = 1.25 October 24, 2016 Roberto Gonzalez Orbital ATK Team A

  5. FIRST DESIGN OPTIONS: Press Band Internal Locking Clamps Rubber Band Contracting System October 24, 2016 Sage Pasternacki & Roberto Gonzalez Orbital ATK Team A

  6. SELECTION PROCESS-PUGH CHART October 24, 2016 Sage Pasternacki Orbital ATK Team A

  7. SELECTION PROCESS-DECISION MATRIX Criteria W.T. Internal Bolt Rubber Band J-Clamps Press Band Polymagnets Locking System Clamp Score W.S. Score W.S. Score W.S. Score W.S. Score W.S. Score W.S. Material 15 4 60 10 150 6 90 10 150 5 75 6 90 Homogeny Material Cost 10 6 60 8 80 4 40 8 80 6 60 7 70 In-House 20 6 120 8 160 6 120 8 160 4 80 7 140 Manufacturability Potential Weight 15 3 45 5 75 2 30 6 90 3 45 10 150 System 20 5 100 9 180 5 100 4 80 6 120 4 80 Complexity Separation Force 20 3 60 5 100 3 60 10 200 2 40 5 100 Modulation Total 100 445 745 440 760 420 630 October 24, 2016 Amanda Crawford Orbital ATK Team A

  8. PRELIMINARY OPTION 1: J-CLAMP October 24, 2016 Garrett Wright Orbital ATK Team A

  9. PRELIMINARY OPTION 2: BOLT October 24, 2016 Amanda Crawford Orbital ATK Team A

  10. PRELIMINARY OPTION 3: POLYMAGNETS October 24, 2016 Christian Johnson Orbital ATK Team A

  11. SCHEDULE October 24, 2016 Garrett Wright Orbital ATK Team A

  12. BUDGET Anticipated Expenses: Quantity Cost Total Cost Round trips to Chandler, AZ 2 $50.00 $100.00 Rental Cost (1 car) 2 $40.00 $80.00 Motor 2 $100.00 $200.00 (For demonstration purposes) Prototype Material $4,949.00 $4,949.00 TOTAL $4,969.00 Current Expenses: Quantity Cost Total Cost Round trip to Chandler, AZ 1 $31.00 $31.00 TOTAL $31.00 RESULTING BUDGET $4,969.00 October 24, 2016 Christian Johnson Orbital ATK Team A

  13. CONCLUSION AND QUESTIONS ➢ Project Description ➢ Design Options ➢ Selection Process ➢ Preliminary Options ➢ Work to be Completed ➢ Conclusion and Questions October 24, 2016 Roberto Gonzalez Orbital ATK Team A

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