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MCCS_SI_05: PI Patch panel ICD and Aircraft Power

MCCS_SI_05: PI Patch panel ICD and Aircraft Power. Erin Smith SITR – 19 February 2010. MCCS_SI_05. Describes the ‘PI Patch panel’ Resulted from the combination of MCCS_SI_03 & MCCS_SI_02 Document reflects implementation of the known Fully Operational Capacity (FOC)

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MCCS_SI_05: PI Patch panel ICD and Aircraft Power

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  1. MCCS_SI_05: PI Patch panel ICD and Aircraft Power Erin Smith SITR – 19 February 2010

  2. MCCS_SI_05 • Describes the ‘PI Patch panel’ • Resulted from the combination of MCCS_SI_03 & MCCS_SI_02 • Document reflects implementation of the known Fully Operational Capacity (FOC) • Additional capability may be added to spare pins on Patch Panel • MCCS_SI_05 now covers both the ‘MCCS to PI rack’ and ‘SI’ sides of the PI Patch Panel

  3. MCCS_SI_02 MCCS_SI_05 MCCS_SI_03

  4. Ground Studs Aircraft FORWARD SI and Counterweight Rack at the TA PI Rack MCCS

  5. MCCS Side • PI Patch Panel to MCCS Physical and Electrical Interface • Power Interface • Network Interface • Audio Interface • Video Interface • Sensors and GPS Antenna Interface

  6. Frequency converter UPS 50 KHz Emergency disconnect Fiber pairs for experimenters network/video network switch Tx Rx 100/1000BASE-FX Fiber pairs for VDS Not used Fiber pairs for MADS

  7. SI Side • PI Patch Panel To Science Instrument Physical and Electrical Interface • Communication lines • Signal lines • Power lines • High voltage (GREAT will eventually need for mid- & high-frequency channels)

  8. Coax N-type connector Coax BNC connector Fiber pair to SI patch panel 75 ohm Coax BNC connector 60 Hz power to SI/CWR

  9. ICD changes

  10. On-aircraft Power Supply

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