1. Team: Juan Pablo Pods System:Modular Aircraft Exterior Pods Strategic Values/Objectives Inexpensive Low Certification Costs Quick Reaction Capable Universal Interfaces Uses New-to-Market Technologies Descriptive Statement The MAEP is a common design allowing for a large variety of units to be installed in a standard rack. The standard rack allows for the interchangeability of a large numbers of sensors, units, and antennas. The common pod design creates a low cost, fast turnaround FAA Certified design, creating a true Quick Reaction Capability effort. Team Members Cody Clanton Brian Claussen Josh Cory Chris Leroux

2. RS Analysis for Modular Aircraft Exterior Pods Correction Variation Reconfigu- ration Expansion (and Contraction of Capacity) Migration Improvement Modification (Add/Sub Capability) Creation (and Elimination) Proactive Reactive Change Domain Response Issues What types of resource relationship configurations will need changed during operation? Modifications to the configuration plan What performance characteristics will the system be expected to improve during operational life cycle? Maximum Weight Maximum Electrical Power What must the system be creating or eliminating in the course of its operational activity? The plan for what components will be needed The creation of a configuration plan for the pod What major events coming down the road will require a change in the system infrastructure? New Materials requiring new manufacturing tools Different Radome Shape What modifications in resources-employed might need made as the system is used? Rack Layout LRU Advancements What can go wrong that will need an automatic systemic detection and response? Failed FAA Certification Inaccurate configuration plan What process variables will range across what values and need accommodation? Environmental Variations What are “quantity-based” elastic-capacity needs on resources/output/activity/other? Different Sized Compartments Variety of electrical power requirements LRU Heating/Cooling demands

3. Reconfigurable Scalable Reusable Encapsulated Modules Component Support (How units are installed in the POD) Radome A/C Interface Mount (How the units interface with the airframe) Power Modules (How power is distributed) Data Bus Heating/Cooling Facilitated Interfacing (Pluggable) Standardized & removable connections Adjustable Rack Space Facilitated Reuse Standardized & removable connections Peer-Peer Interaction Data Bus Deferred Commitment Stubs Certifying to maximum weights Certifying a maximum power feed Evolving Infrastructure Standards Weight Limitations Center of Gravity Configuration Plans Redundancy and Diversity Duplicate Electrical Connections Elastic Capacity Additive Power Modules Data bus capacity Mounting Interface Varieties Heating/Cooling Capacity Distributed Control & Information System user input (User input drives configurations) Vendor input (New Technologies in work) Self-Organization Data bus failure compensation Power module isolation RRS Principles for System: MAEP

4. Modular Aircraft Exterior Pods Component Supports A/C Interface Mount RadomePower Modules Data BusHeating/Cooling Infrastructure evolution System assembly Module mix evolution Module inventory readiness Infrastructure Recon Capable Offensive CapableBroadcast Capable Components/Modules Rules/Standards Integrity Management Active Passive Sockets Signals Security Safety Service Research Eng Engineer/HDL Purchasing Program Manager Aircraft & Module Intf Power & Data Flow ITAR/Classification LVLs FAA & Company Regs Configuration Rules & Conops

5. System: Modular Aircraft Exterior Pods Encapsulated Modules Component Support Radome A/C Interface Mount Power Modules Data Bus Heating/Cooling Evolving Infrastructure Standards Airframe Weight Limit Airframe Total Power Available Center of Gravity Limits Scalable Reusable Missing: Sockets Signals Security Safety Service But you had them on prior slide

6. Proactive Reactive General Issues Create user adaptable experience (Creation) Adjustable Shelving (Modification) Range of acceptable weights (Modification) Range of acceptable power draws (Modification) Maximum Allowable Weight (Improvement) Maximum Allowable Power (Improvement) Radome Materials LRU Improvements LRU Failure (Correction) Environmental Variation (Variation) Pod Damage (Correction) Rack Damage (Correction) Power overdraw (Correction) Weight overload (Correction) LRU Location (Reconfiguration) System: Modular Aircraft Exterior Pods

7. Reality Factors Organizational Behavior – Survival rules rule, nobody's in absolute control... Marketing overselling capabilities Drive to reduce NRE to maximize profits Shortsightedness caused by the need to react quickly. Human (Including Customer) Behavior – Human error, whimsy, expediency, arrogance... Inattention during manufacture and installation Operating outside standard parameters (in hostile environments) Altering maintenance procedures to save time Technology Pace – Accelerating technology and security-vulnerability introductions, sparse testing... COTS Technology advancements (Pushing the operating limits of the pods) GFE requirements driving unexpected configurations System Complexity – Incomprehensible, highly networked, unintended consequences, emergence... Non-intuitive installation and repair procedures Composite material composition and fabrication procedures Globalization – Partners with different ethics, values, infrastructures, cultural assumptions... Different outlooks on acceptable technology use (spying versus justified surveillance) Agile Customers/Competitors/Adversaries – Distributed, collaborative, self organizing, proactive, impatient, innovative... Competitors capable of fully in-house operations Reliant on OEM A/C data Customer desires versus STC Capabilities (One radome design per STC) Partially-Agile Enterprise Faddish Practices – Outsourcing, web services, transparency, COTS policies/affects... Outsourcing composites radome manufacturing and complex machine practices Using COTS (Reliant on vendor priorities) System: Modular Aircraft Exterior Pods

8. Strategic Values/Objectives Functional Activity Strategic Activity ConOps Web LowCertificationCosts Plug and PlayCapabilities Field Modifiable Universal Interfaces Field Maintainable Inexpensive QuickReactionCapable Pre-Analyzed Design Envelopes Uses New- To-MarketTech Standardized Pods System: Modular Aircraft Exterior Pods Use of COTS Technology

9. Adaptive Tool Control & Config Equipment Cross- Certification Field-Wide Processes Continuous/ Recurring Training Adaptable Process Cross Training Facility Support Equipment Continuous Process Research TotalMaintenanceSolution AcceptsMultipleAirframes System: Agile Aircraft Depot Maintenance Operations – Josh Cory QRCCapable Strategic Values/Objectives Functional Activity Strategic Activity ConOps Web

10. Promotes Knowledge Growth Quick Response to Issues High Employee Moral/ Self- Esteem Promotes Open Communica tion Knowledge Database Working Pairs Facilitates Innovative Solutions Current Problem Forum Swarms Employee Recognition for Contributio ns System: Agile Work Force– Chris Leroux

11. Strategic Values/Objectives Functional Activity Strategic Activity ConOps Web Interchange Modules Configure Various Systems System: Maritime Modular Mission Vehicle – Brian Claussen Provide Various Configurations Continue Upgrade Modules Support Multiple MultipleCustomers MeetCustomerNeeds Quick To Market