Safran DSI - eZ Viewer Mission Debriefing Software
eZ Viewer is a data post-flight replay software for use with mission data based on IRIG-106 Chapter 10 format, recorded on ENERTEC recorder/server. This software is an easy-to-use, quick setup and intuitive tool targeted for data replay.
Key Features Comprehensive software tool for:
- Configuration of mission debriefing post-flight debriefing / mission analysis
- Data from on the media or archived
Intuitive interface:
- Pre-configuration of display
- Easy to use and quick setup
- SQUADRON mode
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Available Sources |
Chapter 10 data file(s) Chapter 10 UDP streaming STANAG 4575 volume(s) |
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Chapter 10 Data Types |
Video (Up to 8 channels) MIL-STD-1553 (Up to 8 channels) And additional digital buses |
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Compatibility |
ENERTEC Chapter 10 files ENERTEC Chapter 10 UDP stream Third party Chapter 10 files |
More Product Information
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Equipped with a common L/S/C radiating front end, it’s complemented by a modular set of active RF modules, enabling simultaneous reception and tracking across various frequency bands. Its compact, lightweight design allows it to be mounted on any dishes ranging from 6 to 24 feet.
Available in single, dual, or tri-band configurations, this feed offers the best value for customers looking to meet current requirements while staying future-ready.
It’s also field-upgradable to add any missing bands with straightforward RF module additions, ensuring scalability while keeping costs in check.
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Auto gain (manual gain control: 0 to 32 dB)
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Auto exposure (manual exposure control: 10 µs to 26.8 s)
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Auto white balance (GT3300C only)
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Binning (horizontal and vertical)
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Color correction, hue, saturation (GT3300C only)
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Column defect masking
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Decimation X/Y
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Gamma correction
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Three look-up tables (LUTs)
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Region of interest (ROI), separate ROI for auto features
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Reverse X/Y
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P-Iris and DC-Iris lens control
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Event channel
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Image chunk data
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IEEE 1588 Precision Time Protocol (PTP)
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RS232
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Storable user sets
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StreamBytesPerSecond (bandwidth control)
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Stream hold
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Sync out modes: Trigger ready, input, exposing, readout, imaging, strobe, GPO
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Tap mode switchable in Vimba Viewer 2.0 or later (four-tap, one-tap)
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Temperature monitoring (main board and sensor board)
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Trigger over Ethernet (ToE) Action Commands
The MDR system is your key to data collection in challenging, real-world airborne flight test scenarios. Its modular design allows it to seamlessly adapt to the full spectrum of test requirements, whether it’s a lightweight task or an extensive mission with diverse signals, environmental challenges, and lengthy recording periods.
A comprehensive range of signal interface modules, custom-tailored for various data sources and bus types, ensures that it’s ready to meet today’s demands and future requirements.
The VS1410 is a video & data recorder/server packaged in a rugged compact chassis (3.75” x 5.75” x 7.36” / 6.4 lb), for recording on a Removable Memory Module (RMM).
Recorded data can be replayed in a standard PC/Windows® environment, using specific or COTS mission debrief solutions for post mission analysis. In addition, typically for ISR applications, data can be replayed while recording on board.
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These units are suitable for both manned and unmanned ground, air, and sea vehicles. They undergo rigorous validation and formal qualification testing, adhering to standard test methods such as DO-160 and MIL-STD-810.
The PPS®X00 plasma thruster (Hall effect) takes benefit of Safran’s long experience with electric propulsion to propose a very efficient product. PPS®X00 was designed to address the specific requirements inherent in the “New Space” market environment. With a lifespan exceeding 5,000 hours and very high specific impulse, the PPS®X00 is an extremely versatile thruster, making it ideal for all types of applications in its core market: low Earth orbit (LEO).
The PPS®1350 Hall Effet plasma thruster draws on Safran’s long experience with electric propulsion. It is designed for orbital transfer, station keeping and deorbiting satellites and other spacecraft. In particular, the PPS 1350 was the primary engine on ESA’s lunar probe, Smart-1, launched in 2003 by an Ariane 5 rocket. This mission was completed in September 2006.
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Auto gain (manual gain control: 0 to 32 dB)
-
Auto exposure (manual exposure control: 10 µs to 26.8 s)
-
Auto white balance (GT1910C only)
-
Binning (horizontal and vertical)
-
Color correction, hue, saturation (GT1910C only)
-
Column defect masking
-
Decimation X/Y
-
Gamma correction
-
Three look-up tables (LUTs)
-
Region of interest (ROI), separate ROI for auto features
-
Reverse X/Y
-
P-Iris and DC-Iris lens control
-
Event channel
-
Image chunk data
-
IEEE 1588 Precision Time Protocol (PTP)
-
RS232
-
Storable user sets
-
StreamBytesPerSecond (bandwidth control)
-
Stream hold
-
Sync out modes: Trigger ready, input, exposing, readout, imaging, strobe, GPO
-
Tap mode switchable in Vimba Viewer 2.0 or later (four-tap, one-tap)
-
Temperature monitoring (main board and sensor board)
-
Trigger over Ethernet (ToE) Action Commands
Safran DSI
Safran DSI Testing & Telemetry provides complete, end-to-end solutions covering instrumentation, mission systems, onboard recording, and transmission, through to base stations for data monitoring and control. Our solutions are platform-agnostic and adaptable to customer mission needs.