Reflections on COTS in Avionics/Vetronics

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    Reflections on COTS in Avionics/Vetronics - Presentation Transcript

    1. Reflections on COTS in Avionics/Vetronics The Use of COTS Assemblies in Harsh Environment Two-Level Maintenance Systems – May 12 th , 2005 James A. Robles, Senior Technical Fellow The Boeing Company Phn: (206) 655-9062 Email: [email_address] BOE 042105-077
    2. Context – The Environment Changed We Won the Cold War Control of the Electronics Industry Acquisition Reform New Generation of Users
      • 1994 Perry Memo
      • Streamline procurement of reduce cycle time and cost
      • Strengthen technology/industrial base
      • Increased access to advanced technologies
      • Move away from the military specification system
      • Not My Generation
      • Better educated and more aware of technology
      • Not willing to tackle a difficult job with obsolete hardware
      • Useful life reduced to correspond to desired technology refresh cycle
      Defense Outlays As a Share of Gross Domestic Product 2 4 6 8 10 12 50 60 70 80 90 00 3.0 GDP (%) 4.4 4.7 11.9% 9.1% 6.3% Year
    3. What My Customers Require on Advanced Fighters, Helicopters, and Ground Vehicles
      • Minimize Total Ownership Cost (TOC)
        • Development Cost
        • Unit Recurring Flyaway (URF) Cost
        • Operation and Support (O&S) Cost
      • High functional density to minimize weight and volume
        • Thermal density (watts/cm)
      • Perform reliably in harsh environment
        • Reduce thermal strains to improve inherent reliability
        • Uniformity of temperature distribution across module
        • Exposure to coolant
        • Complexity
      • Compatibility with two-level maintenance
      • Facilitate insertion of new technology and mitigation of component obsolescence
        • Thermal margin
    4. Obstacles to Wider Usage of Available COTS
      • Low Functional Density
      • Current standards do not meet the need
        • IEEE 1101.1 Air Cooled
        • IEEE 1101.2 Conduction Cooled
      • Not Compatible with Two-Level Maintenance Requires an ESD protected connector and covers for handling protection
        • Two to three times O&S cost penalty
        • F/A-22 example
      • Lack of a Standard for Environments
      • A Gaping hole in our “open architectures’
        • Exposes programs to risk with each DMS fix or upgrade cycle
    5. Enablers for Wider Usage of Tomorrow’s COTS
      • Higher Functional Density
      • Standards under development will meet the need
        • VITA 46
        • VITA 48
      • Compatible with Two-Level Maintenance
      • VITA 46 and VITA 48 will have an ESD protected connector
      • VITA 48 will provide optional covers for ESD and handling
      • We Have a Standard for Environments
      • Fills the gaping hole in our “open architectures’
        • ANSI VITA 47 is released
    6. The Thermal Management Challenge and Answer
      • Thermal management challenge
        • More heat to remove
        • Less “potential” to drive it out
      • Consequences
        • Unit Recurring Flyaway cost
        • Functional density – fuel cost (O&S cost), lethality, survivability.
        • Reliability (O&S cost)
        • Margin for DMS fixes
        • Margin for technology insertion
      • The answer --- VITA 48
        • Enhanced conduction cooling
        • Liquid Flow Through Cooling
        • Spray Cooling
      BOE 042105-077
    7. Outlook for the Future
      • We are addressing the obstacles to wider usage of COTS assemblies in avionics/vetronics
      • The environment will continue to change in ways that encourage the use of COTS
      • We are at a tipping point – much wider use of COTS assemblies in harsh environment two-level maintenance systems
    8.  

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