Qualified, certifiable
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ROHS, RTCA, DO-160, others on request
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ROHS, RTCA, DO-160, NSRP qualified program: NASA Sounding Rocket Operations
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ROHS, RTCA, DO-160, others on request
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ROHS, RTCA, DO-160, others on request
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Environments
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Indoor/Outdoor
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Indoor/Outdoor/ Vacuum
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Indoor/Outdoor
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Indoor/Outdoor
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References / Application proof
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FTI for fixed wings aircraft and rotary wings, crash recording for light aircraft and helicopters, UAVs, VTOL / air taxi, training, debriefing and recording; surveillance for cockpit and external cargo
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Space & launcher applications
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UAV piloting for HALE, MALE, VTOL, Super sonic harsh aerial vehicles; FTI; taxiing
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UAV piloting; FTI (standard item for Airbus); transport aircraft; AAR; taxiing
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OS / Interfaces
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Embedded Linux, IP Ethernet / FTP access
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Embedded Linux, IP Ethernet / FTP access
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Embedded Linux, IP Ethernet / FTP access, INET-X
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HD-SDI, SD-SDI, RS422/232
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Sensors
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CMOS, global shutter
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CMOS, global shutter
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CCD, global shutter, color (monochrome on request)
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CCD, global shutter, color (monochrome on request)
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Resolution
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up to Full HD 1080p60
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up to Full HD 1080p60
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Dual video streams: Full HD 1920x1080p30, 640x360p30
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HD-SDI, HDTV, 1920x1080p25
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Control interface
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GeniCam, XML Files (Control), GigE Vision, optional: SferiRec® (FE 320 LCR)
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GeniCam, XML-Files (Control), GigE Vision
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GeniCam, XML-files (Control), GigE Vision, MPEG2TS (Data), PoE (Power)
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RS 485, Kappa protocol
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Triggering
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External hardware trigger, software trigger
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External hardware trigger, software trigger
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External hardware trigger
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-
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Time synchronicity
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PTPv2 (IEEE1588)
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PTPv2 (IEEE1588)
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PTPv2 (IEEE1588)
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-
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Latency
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Camera: < 150 ms (Approx. 80 ms between sensor and camera output @ 1080p60)
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Camera: < 150 ms (Approx. 80 ms between sensor and camera output @ 1080p60)
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Glass-to-glass: < 250 ms
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Camera: < 10 ms
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Memory
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Internal SD for loop recording
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Internal SD for loop recording
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-
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-
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Compression
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H.264, 1-16 Mbit/s, dual streaming, high profile (level 5) adjustable
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H.264, 1-16 Mbit/s, dual streaming, high profile (level 5) adjustable
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H.264 compression, 1-16 Mbit/s, dual streaming, high profile (level 5) adjustable
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-
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Interfaces / bandwith
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GigE, 1 Gbit/s
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GigE, 1 Gbit/s
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Ethernet 100 Mbit/s
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HD-SDI, 1.5 Gbit/s
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Frame rate
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1080p60 (60 fps), 720p120 (120 fps), 360p200 (180 fps), adjustable up to 180 fps depending on resolution and imager
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1080p60 (60 fps), 720p120 (120 fps), 360p200 (180 fps), adjustable up to 180 fps depending on resolution and imager
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Adjustable from 1-30 fps
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SD-SDI 50i, HD-SDI 25p
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Dimension / Weight
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CEU (corpus): 59 x 40 x 116 mm (incl. connectors), appr. 360 g; CSU (head): 50 x 39 x 53 mm, appr. 150 g (51° HFoV, excl. heater, incl. lens protection)
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CEU (corpus): 59 x 40 x 116 mm (incl. connectors), appr. 360 g; CSU (head): 50 x 39 x 53 mm, appr. 150 g (51° HFoV, excl. heater, incl. lens protection)
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CEU (corpus): 59 x 40 x 116 mm (incl. connectors), appr. 360 g; CSU (head): 50 x 39 x 53 mm, appr. 150 g (51° HFoV, excl. heater, incl. lens protection)
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Ø 60 x 140mm (excl. Connectors), 620g (depending on model)
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Power supply
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9-36 V DC (compact & remote head version), optional: 9-60 V DC with CPE, power interruption 100ms)
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9-36 V DC (compact & remote head version), optional: 9-60 V DC with CPE, power interruption 100ms)
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MIL-STD 704 A; 18.5-32.5 V DC, galvanic isolation
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MIL-STD 704 A, 15-50 V DC, galvanic isolation
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De-icing / De-misting system
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Optional
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Optional
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Built-in
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Built-in
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Specials
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Modular concept, flexible with remote head, distance up to 10m, active-wire, COTS, ITAR-free
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Tested in vacuum and for extended shock & vibration conditions for space application. NASA-tested ME40280 environmental test, COTS, ITAR free
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easy integration in any electrical environment with power peak and power gap protection (250 ms), COTS, ITAR free
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Standard camera for AIRBUS FTI, COTS, ITAR free
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