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ERAU ASCEND! STRUCTURES AND SYSTEMS INTEGRATION Nicholas Hammons
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ERAU ASCEND! STRUCTURES and SYSTEMS INTEGRATION

Feb 23, 2016

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ERAU ASCEND! STRUCTURES and SYSTEMS INTEGRATION. Nicholas Hammons. PREVIOUS STRUCTURE. Fold-out poster board mounting Carbon fiber-epoxy lid External GPS Velcro mounting Inseparable subsystems Wiring mess. GOALS. Improve component accessibility Separate subsystems Reduce wiring mess - PowerPoint PPT Presentation
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Page 1: ERAU ASCEND! STRUCTURES and SYSTEMS INTEGRATION

ERAU ASCEND!STRUCTURES AND SYSTEMS

INTEGRATIONNicholas Hammons

Page 2: ERAU ASCEND! STRUCTURES and SYSTEMS INTEGRATION

PREVIOUS STRUCTURE Fold-out poster board

mounting Carbon fiber-epoxy lid

External GPS Velcro mounting Inseparable

subsystems Wiring mess

Page 3: ERAU ASCEND! STRUCTURES and SYSTEMS INTEGRATION

GOALS Improve component accessibility Separate subsystems Reduce wiring mess Internalize GPS antenna Integrate PICAXE microcontroller Add solar cell module Lighten payload (< 4 lbs)

Page 4: ERAU ASCEND! STRUCTURES and SYSTEMS INTEGRATION

SOLUTIONS Accessibility: Slide-out flanges Sys. Separation: Separate power

systemsSeparate levels

Wiring: Ribbon cable/connectors

GPS: Glass-epoxy lid PICAXE: Data board Solar Cells: Lid-mounted module Weight: Composites

Page 5: ERAU ASCEND! STRUCTURES and SYSTEMS INTEGRATION

CURRENT PAYLOAD STUCTURE Shell Lid Shelving System

APRS Layer Data Collection

Layer

Page 6: ERAU ASCEND! STRUCTURES and SYSTEMS INTEGRATION

PAYLOAD SHELL Inherited/reusable

shell 5 launches

8” x 8” x 8” cube Bi-directional carbon

fiber ¼” foam core External access to

on/off switches ~ 421 in3 useable

volume

Page 7: ERAU ASCEND! STRUCTURES and SYSTEMS INTEGRATION

PAYLOAD LID Glass-epoxy

GPS transmission ¼” foam core GPS antenna/ground

plane mounted internally Solar cells mounting Silicon gel to reduce heat

flux

Page 8: ERAU ASCEND! STRUCTURES and SYSTEMS INTEGRATION

SOLAR CELL MODULE Glass-epoxy ¼” foam core Plexiglas cover

Page 9: ERAU ASCEND! STRUCTURES and SYSTEMS INTEGRATION

SHELVING SYSTEM Mimic EYASSAT NanoSat

Modules Separate power

requirements Carbon fiber-epoxy laminate

Slide-out flanges: 3-ply Brackets: 2-ply

Reduces structure volume and weight ~ 7.5% more internal

volume(vs. Nov. 22, 2008 launch)

Page 10: ERAU ASCEND! STRUCTURES and SYSTEMS INTEGRATION

APRS LAYER TinyTrak 4 Radio GPS Evaluation

Board Voltage Regulator AA Battery Pack

Page 11: ERAU ASCEND! STRUCTURES and SYSTEMS INTEGRATION

DATA COLLECTION LAYER ¼” foam core Data board:

PICAXE Logomatic Voltage

Regulator Internal/External

Temperature Sensors

Pressure Sensor AA Battery Pack

Page 12: ERAU ASCEND! STRUCTURES and SYSTEMS INTEGRATION

SYSTEM INTEGRATION Velcro mounting 1 cross-board

connection On/off switch

2 lid to payload connections Solar cells GPS antenna

External on/off switches Payload weight at

launch: 3 lbs 11 oz

Page 13: ERAU ASCEND! STRUCTURES and SYSTEMS INTEGRATION

FUTURE IMPROVEMENTS Integrate data collection system into PC

boards Convertible payload Reduce APRS volume to maximize space for

collecting data

Fabricate sun sensor module

Improve thermal regulation

Page 14: ERAU ASCEND! STRUCTURES and SYSTEMS INTEGRATION

QUESTIONS

Page 15: ERAU ASCEND! STRUCTURES and SYSTEMS INTEGRATION

ATTITUDE DETERMINATION

Andrew Grant