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美国防空手册部分章节(6) 

(2007-12-25 02:23:24)
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军事

  美国防空手册部分章节(6) 
 
 
 

Mission Application Program

  1. The Mission Application Program (MAP) provides real-time mission processing to satisfy all mission needs. MAP computes search rosters, plans radar activities for targets and interceptors and generates all radar transmit and receive timeline plans. MAP implements the radar timeline plan and generates the required radar action commands. MAP sorts radar returns, corrects detection, and performs radar status checks. MAP performs target track initiation, return-to-track correlation and track update. MAP maintains the radar-to-interceptor interface. MAP does launch and impact point determination for targets in track, performs target classification, jammer processing and kill assessment.

    Pre-and Post-Processing Support Software

  2. A collection of non-real-time tools that produce mission profiles, compute and store radar data calibration constants, and support post mission performance analysis.

    Radar Test Control Program

  3. This software is an integrated set of diagnostic tests which provide the ability to assess overall system status, control embedded hardware configuration item testing, support failure isolation and repair to the line replaceable unit level and aid in the isolation of subtle, system level irregularities. It presents an operator interface supporting system level objectives of rapid diagnostics and repair. The software operates in two modes: off-line under operator control to support maintenance operations and on-line in coordination with MAP software to perform fault detection during mission operation.

    Radar Simulation Software

  4. This software is a integration, development, and readiness verification tool which allows the MAP software to be tested in real-time using scenarios expected in actual operation. It operates in three modes: digital, analog and signal processor. In the digital mode, the software simulates the threat environment, external messages and all radar hardware. In the analog mode, the software receives radar action commands from MAP, generates test targets according to a target scenario and generates external messages allowing real-time testing without radiating. In the signal processor mode, MAP and the software act with the signal processor to test the signal processor and its interface to the data processing equipment.

    Display and Control Program

  5. This software supports the soldier-machine interface to the radar.

    External Communications Program

  6. This software supports all data communications from the THAAD radar.

    Cooling Equipment Unit

  7. The Cooling Equipment Unit (CEU) provides liquid cooling required for the AE. In addition, it houses the main power distribution unit for the EEU and AE. The trailer has an air-ride suspension on both the main dolly set and the kingpin mechanism. The coolant lines have quick disconnect fittings for rapid march order and emplacement. A status panel with alarm center provides status and warning of coolant overheating and fan failure. The CEU also has low coolant pressure and coolant reservoir level indicators. A low temperature, oil-fired boiler provides for fast equipment start-up. The cooling system contains a 50-gallon reservoir capacity and features an air separator for rapid voiding of air prior to supplying coolant to the AE (figure 4-4).
    http://www.fas.org/spp/starwars/docops/fm44-100-2fd/4-04.gif
    Figure 4-4. Cooling Equipment Unit

  8. The prime power unit (PPU) is a diesel engine generator set with a capacity of 1.1 megawatts of continuous 4160-volt, 3-phase power for the radar. The PPU is configured on a semi-trailer pulled by the M983 tractor. The PPU operates on approximately 90 gallons per hour of JP8 fuel. The PPU has storage capacity for one hour of operation, and interfaces with tankers for extended operations. Power is output to the power distribution unit on the CEU that distributes power to the AE and EEU. Power may also be provided to the Operator Control Unit (OCU), but normally the PU801 powers the OCU. Commercial power may be provided to the main power distribution power in lieu of PPU power (figure 4-5).

    Operator Control Unit

  9. The Operator Control Unit (OCU) contains three workstations for control and monitoring of the radar. The OCU interfaces with BMC3I, and is housed in a lightweight shelter that is mounted on a HMWWV. The shelter has a gas particulate filter unit (GPFU) and an NBC enclosure. The system has an uninterruptible power supply (UPS), to safely power down the system in the event of loss of prime power. The towed PU801 15-kw generator set powers the OCU. It may also be powered by the PPU via the CEU power distribution unit. A fiber optics cable connects the OCU to the EEU. The OCU with PU801 is C141 roll-on/roll-off capable. The OCU functions will be incorporated into the electronics equipment unit in the objective battalions.
    http://www.fas.org/spp/starwars/docops/fm44-100-2fd/4-04.gif
    Figure 4-5. Prime Power Unit

    Battle Management/Command, Control, Communications, and Intelligence (BMC3I)

  10. The BM/C3I is the battle management component of the THAAD system. Battle Management/Command, Control, Communications, and Intelligence (BMC3I) consist of two major components: the Tactical Operations Station (TOS), and the Launch Control Station (LCS). The TOS and LCS are HMMWV-mounted shelters that are powered by trailer-mounted 15-kw generators (PU-801). Both have identical environmental control units and Gas Particulate Filter Units (GPFU) providing NBC protection.

  11. A Tactical Shelter Group (TSG) is composed of a Tactical Operations Station (TOS), a Launch Control Station (LCS), an antenna/Cable Vehicle (ACV), and three generators.

    Tactical Operations Station

  12. The TOS equipment consists of a central processor computer, two operator workstations, data storage devices, a printer, and facsimile equipment. The TOS exchanges data and voice with the LCS via a high capacity dual fiber distributed data interface LAN. The fiber-optic lines carry data and voice communications to the LCS. The TOS also has a DNVT telephone that provides full duplex voice or data, non-cryptographic communications connection to the MSE equipment. A laser printer provides quality hard copy print out in black and white or color. An ECU provides environment control function selection and station temperature control.

  13. The GPFU shelter provides ON/OFF power control, audible alarm, and fault indications related to air pressure monitoring during life-endangering environments involving NBC threats. The uninterruptible power supply (UPS) provides a backup power source used when the primary power to the shelter is interrupted. It allows the operator 10 to 14 minutes to perform an orderly shutdown of equipment to prevent damage. Additionally, the circuit breaker provides ON/OFF power control and overcurrent protection for TOS equipment.

  14. A communication interface unit (CIU) provides automatic analog/digital voice switching controlled by the central computer. The CIU also interfaces the VCCM, loop nest, DNVT, and FAX. The central computer provides the interface to the CIU and the fiber optic subsystem. The voice communications control monitor provides operator access for voice intercommunications and radio/wire communications to external agencies.
    http://www.fas.org/spp/starwars/docops/fm44-100-2fd/4-06.gif
    Figure 4-6. Tactical Operations Station (Inside configuration of equipment may change as development progresses)

    Launch Control Station

  15. The LCS provides the automated digital data transfer and voice communications interfaces. All components of the radio subsystem are located in or on the LCS except for the ground-mounted antennas. The extensive communications suite consists of a JTIDS terminal, Army common user system interface equipment/mobile subscriber equipment (ACUS/MSE) interface equipment, single channel ground and airborne radio system (SINCGARS), a commander's tactical terminal-hybrid receiver (CTT/H-R), a precision lightweight global positioning system receiver (PLGR) and crypto-secure equipment. The voice communications subsystem (VCS) equipment is a switching system that provides an interface to communications equipment both internal and external to the TSG.

  16. The LCS has a roof-mounted dual batwing antenna for the CTT/H-R terminal. There are four ground-mounted antennas for the SINCGARS VHF radio sets and for the PLGR. Externally, the communications demarcation panel provides the cable connections between the LCS and external DNVT. In addition, it provides electromagnetic interference /electromagnetic compatibility (EMI/EMC) filtering.
    http://www.fas.org/spp/starwars/docops/fm44-100-2fd/4-07.gif
    Figure 4-7. Launch Control Station 

    Mission Application Program

    1. The Mission Application Program (MAP) provides real-time mission processing to satisfy all mission needs. MAP computes search rosters, plans radar activities for targets and interceptors and generates all radar transmit and receive timeline plans. MAP implements the radar timeline plan and generates the required radar action commands. MAP sorts radar returns, corrects detection, and performs radar status checks. MAP performs target track initiation, return-to-track correlation and track update. MAP maintains the radar-to-interceptor interface. MAP does launch and impact point determination for targets in track, performs target classification, jammer processing and kill assessment.

      Pre-and Post-Processing Support Software

    2. A collection of non-real-time tools that produce mission profiles, compute and store radar data calibration constants, and support post mission performance analysis.

      Radar Test Control Program

    3. This software is an integrated set of diagnostic tests which provide the ability to assess overall system status, control embedded hardware configuration item testing, support failure isolation and repair to the line replaceable unit level and aid in the isolation of subtle, system level irregularities. It presents an operator interface supporting system level objectives of rapid diagnostics and repair. The software operates in two modes: off-line under operator control to support maintenance operations and on-line in coordination with MAP software to perform fault detection during mission operation.

      Radar Simulation Software

    4. This software is a integration, development, and readiness verification tool which allows the MAP software to be tested in real-time using scenarios expected in actual operation. It operates in three modes: digital, analog and signal processor. In the digital mode, the software simulates the threat environment, external messages and all radar hardware. In the analog mode, the software receives radar action commands from MAP, generates test targets according to a target scenario and generates external messages allowing real-time testing without radiating. In the signal processor mode, MAP and the software act with the signal processor to test the signal processor and its interface to the data processing equipment.

      Display and Control Program

    5. This software supports the soldier-machine interface to the radar.

      External Communications Program

    6. This software supports all data communications from the THAAD radar.

      Cooling Equipment Unit

    7. The Cooling Equipment Unit (CEU) provides liquid cooling required for the AE. In addition, it houses the main power distribution unit for the EEU and AE. The trailer has an air-ride suspension on both the main dolly set and the kingpin mechanism. The coolant lines have quick disconnect fittings for rapid march order and emplacement. A status panel with alarm center provides status and warning of coolant overheating and fan failure. The CEU also has low coolant pressure and coolant reservoir level indicators. A low temperature, oil-fired boiler provides for fast equipment start-up. The cooling system contains a 50-gallon reservoir capacity and features an air separator for rapid voiding of air prior to supplying coolant to the AE (figure 4-4).
      http://www.fas.org/spp/starwars/docops/fm44-100-2fd/4-04.gif
      Figure 4-4. Cooling Equipment Unit

    8. The prime power unit (PPU) is a diesel engine generator set with a capacity of 1.1 megawatts of continuous 4160-volt, 3-phase power for the radar. The PPU is configured on a semi-trailer pulled by the M983 tractor. The PPU operates on approximately 90 gallons per hour of JP8 fuel. The PPU has storage capacity for one hour of operation, and interfaces with tankers for extended operations. Power is output to the power distribution unit on the CEU that distributes power to the AE and EEU. Power may also be provided to the Operator Control Unit (OCU), but normally the PU801 powers the OCU. Commercial power may be provided to the main power distribution power in lieu of PPU power (figure 4-5).

      Operator Control Unit

    9. The Operator Control Unit (OCU) contains three workstations for control and monitoring of the radar. The OCU interfaces with BMC3I, and is housed in a lightweight shelter that is mounted on a HMWWV. The shelter has a gas particulate filter unit (GPFU) and an NBC enclosure. The system has an uninterruptible power supply (UPS), to safely power down the system in the event of loss of prime power. The towed PU801 15-kw generator set powers the OCU. It may also be powered by the PPU via the CEU power distribution unit. A fiber optics cable connects the OCU to the EEU. The OCU with PU801 is C141 roll-on/roll-off capable. The OCU functions will be incorporated into the electronics equipment unit in the objective battalions.
      http://www.fas.org/spp/starwars/docops/fm44-100-2fd/4-04.gif
      Figure 4-5. Prime Power Unit

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