1. Be P16102 Constrain Subsystems House Internals Provide Access Mount components securely Stow Solar Panels Gather Solar Energy Expose Panels before Deployment Deploy Array Unfold Structure Extend Structure Maintain Shape Structure Follow Sun Know Earth, Sun, Sat Geometry Turn Array Perform “Mission” Meet CSLI Requirements Meet $ Requirements Survive “Mission” Survive Launch Get Shook Up Integrate into PPOD Deploy from PPOD Survive Orbit Environment Manage Heat Minimize Change of Inertial Properties

2. Be P16102 Constrain Subsystems House Internals Provide Access Mount components securely Stow Solar Panels Gather Solar Energy Expose Panels before Deployment Deploy Array Unfold Structure Extend Structure Maintain Shape Structure Follow Sun Perform “Mission” Meet CSLI Requirements Meet $ Requirements Survive “Mission” Survive Launch Get Shook Up Integrate into PPOD Deploy from PPOD Survive Orbit Environment Manage Heat Minimize Change of Inertial Properties

3. Be P16102 Constrain Subsystems House Internals Provide Access Mount components securely Stow Solar Panels Gather Solar Energy Expose Panels before Deployment Deploy Array Unfold Structure Extend Structure Maintain Shape Structure Follow Sun Perform “Mission” Meet CSLI Requirements Meet $ Requirements Survive “Mission” Survive Launch Get Shook Up Integrate into PPOD Deploy from PPOD Survive Orbit Environment Manage Heat Minimize Change of Inertial Properties Structure Deployment Mechanism Deployed Structure All

4. CubeSat P16102 Structure Deployment Mechanism Deployed Structure Provide Access to Internals Mount components securely Stow Solar Panels Expose Panels before Deployment Unfold/Unlatch Structure Extend Structure Maintain Shape Structure Follow Sun Avionics/ Command ADCS/ Orientation EPS/ Power Command Power Mech. Linkage

5. Be P16102 Constrain Subsystems House Internals Provide Access Mount components securely Stow Solar Panels Gather Solar Energy Expose Panels before Deployment Deploy Array Unfold Structure Extend Structure Maintain Shape Structure Follow Sun Perform “Mission” Meet CSLI Requirements Meet $ Requirements Survive “Mission” Survive Launch Vibration Testing Integrate into PPOD Deploy from PPOD Survive Orbit Environment Manage Heat Minimize Change of Inertial Properties ERDescription 1 Minimum Undeployed Area Time 2 Maximum Deployed Area Time 3 System Mass 4 PPOD-CubeSat Clearance 5 Time from command to deploy 6 Operating Temperature 7 Volume Fraction of Structure 8 Change in Center of Mass 9 Cost of Prototype 10 Time to remove PCB Blank 11 Launch Vibration Test from 16103 12 Full documentation of design and CAD package 1 2 3 4 5 6 11 2 7 10 8 9 3 8 11 1