Diren ABAT, mer BATMAZ, Team Leader Design Engineer Defence - - PowerPoint PPT Presentation

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Diren ABAT, mer BATMAZ, Team Leader Design Engineer Defence - - PowerPoint PPT Presentation

Diren ABAT, mer BATMAZ, Team Leader Design Engineer Defence Systems Business Sector, ASELSAN Inc. Defence Systems Business Sector, ASELSAN Inc. Overview Zargana TM System by ASELSAN Outboard Launchers of Zargana TM Estimation of Minimum


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Diren ABAT, Team Leader Defence Systems Business Sector, ASELSAN Inc. Ömer BATMAZ, Design Engineer Defence Systems Business Sector, ASELSAN Inc.

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SLIDE 2

Overview

UDT 2020, Rotterdam 1

ZarganaTM System by ASELSAN Outboard Launchers of ZarganaTM Estimation of Minimum Launching Speed Tests & Measurements Exit Speed Analysis Conclusion

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SLIDE 3

ZarganaTM System by ASELSAN

UDT 2020, Rotterdam 2

  • Host Platform Data Reception

and Processing

  • Threat Data Reception and

Processing

  • Sonar

Data Reception and Processing

  • Data Processing
  • Advise
  • n

Tactical Evasive Maneuver

  • Display and Warning
  • Launcher Control
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Outboard Launchers of ZarganaTM

UDT 2020, Rotterdam 3

  • Instant reaction (< 5s)
  • Separate launchers for port

and starboard

  • Interface with decoys/jammers
  • Automatic programming and

powering of decoys/jammers before deployment

  • High redundancy
  • Silent launch (No bubble /

gas release to environment)

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SLIDE 5

Outboard Launchers of ZarganaTM (cont’d)

UDT 2020, Rotterdam 4

  • Can be configured according to space on submarine

Launcher Unit (LU) Launching Module (LM)

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Outboard Launchers of ZarganaTM (cont’d)

UDT 2020, Rotterdam 5

  • Launching at all operation depths
  • Gas generators are used inside
  • Patented design, no gas and bubble release
  • Decoys/jammers can be programmed just before launch
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SLIDE 7

Estimation of Minimum Launching Speed

UDT 2020, Rotterdam 6

  • Safe separation for an affective soft-kill defense
  • Safe separation must be possible at,
  • All submarine speeds
  • All submarine maneuvers
  • All operation depths
  • Multiple numbers of 6DOF simulations are performed
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SLIDE 8

Estimation of Minimum Launching Speed (cont’d)

UDT 2020, Rotterdam 7

  • Simulation involves submarine maneuvers separately;
  • Heading – Sterning pitch
  • Roll
  • Turning

Also combinations

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Estimation of Minimum Launching Speed (cont’d)

UDT 2020, Rotterdam 8

  • Different launching angles are considered, as well
  • At horizontal plane
  • At vertical plane
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Estimation of Minimum Launching Speed (cont’d)

UDT 2020, Rotterdam 9

  • Approximately the thousand of simulations were run
  • Minimum exit speed was determined
  • Detailed design was proceeded w.r.t. min. decoy exit speed
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SLIDE 11

Tests & Measurements

UDT 2020, Rotterdam 10

  • Launching Unit must be capable of providing min. exit speed to decoy
  • Tests were performed because of
  • To specify Launcher Unit geometry (Volume, nozzle profile, etc.)
  • To determine power of gas generators
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SLIDE 12

Tests & Measurements (cont’d)

UDT 2020, Rotterdam 11

  • How can we measure the exit speed in water?
  • Magnetic field can be used
  • Well designed test equipment and prototypes were produced

Leakproof Magnetic Coil Electronic Box

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Tests & Measurements (cont’d)

UDT 2020, Rotterdam 12

  • Working principle of the test system base on,
  • By means of two magnets on the test decoy
  • Magnetic field of coil is distorted
  • Time step between the two peaks is obtained
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Tests & Measurements (cont’d)

UDT 2020, Rotterdam 13

  • Many water tests were performed up to depth of ~200m
  • Various gas generator types are tried
  • Avg. exit speeds with each gas generator were recorded

Depth (m) Speed (m/s) Gas Generator Configurations 1 23 Configuration 1 50 23,5 Configuration 2 100 17.3 Configuration 3 150 29,2 Configuration 4 180 27 Configuration 5

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SLIDE 15

Exit Speed Analysis

UDT 2020, Rotterdam 14

  • We need exit speed analysis for more than ~200m depth
  • Pressure characteristics of gas generators should be modeled
  • Motion of the decoy during launching should be modeled
  • Model should be corrected according to sea test results
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Exit Speed Analysis (cont’d)

UDT 2020, Rotterdam 15

  • A pressure cylinder with variable inner volume was designed
  • All specified gas generators were tested at each volume
  • Pressure vs. Time graphs are obtained
  • Pressure at the demanded time and volume was put to analysis
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Exit Speed Analysis (cont’d)

UDT 2020, Rotterdam 16

  • Launching process of the decoy was modelled as 4 different phases

Phase-1: Gas generators are activated. The cap of LU is not opened. Phase-2: Cap is opened. Decoy is moving with ram plate and water inside the LU.

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Exit Speed Analysis (cont’d)

UDT 2020, Rotterdam 17

  • Launching process of the decoy was modelled as 4 different phases

Phase-3: Ram plate is stagnant. Decoy is leaving from ram plate. Water is filling remaining volume. Phase-4: Decoy is not inside the LU anymore. It gains its exit speed.

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Conclusion

UDT 2020, Rotterdam 18

  • For a successful countermeasure, safe separation of decoy must be assured
  • Following steps are followed to define desired exit decoy speed
  • All submarine maneuvers were examined with simulation
  • Sea tests were performed and collected data up to limited depth
  • Mathematical model was constituted and corrected according to sea tests
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