Web Developer & Recorder, Primary Author, Project Manager & - - PowerPoint PPT Presentation

Orbital ATK Team A October 24, 2016

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

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

• f 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.

Garrett Wright Orbital ATK Team A October 24, 2016

FUNCTIONAL DECOMPOSITION

Christian Johnson Orbital ATK Team A October 24, 2016

REQUIREMENTS

Roberto Gonzalez Orbital ATK Team A October 24, 2016

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

FIRST DESIGN OPTIONS:

Sage Pasternacki & Roberto Gonzalez Orbital ATK Team A October 24, 2016

Internal Locking Clamps Press Band Rubber Band Contracting System

SELECTION PROCESS-PUGH CHART

Sage Pasternacki Orbital ATK Team A October 24, 2016

SELECTION PROCESS-DECISION MATRIX

Amanda Crawford Orbital ATK Team A October 24, 2016

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

PRELIMINARY OPTION 1: J-CLAMP

Garrett Wright Orbital ATK Team A October 24, 2016

PRELIMINARY OPTION 2: BOLT

Amanda Crawford Orbital ATK Team A October 24, 2016

PRELIMINARY OPTION 3: POLYMAGNETS

Christian Johnson Orbital ATK Team A October 24, 2016

SCHEDULE

Garrett Wright Orbital ATK Team A October 24, 2016

BUDGET

Christian Johnson Orbital ATK Team A October 24, 2016

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 (For demonstration purposes) 2 $100.00 $200.00 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

CONCLUSION AND QUESTIONS

Roberto Gonzalez Orbital ATK Team A October 24, 2016

➢Project Description

➢Design Options ➢Selection Process ➢Preliminary Options ➢Work to be Completed ➢Conclusion and Questions