Nuvia法国机载综合辐射监测系统AIRIS
AIRIS 专为基于伽马光谱的机载辐射测量而设计。该系统可以安装在固定翼和直升机平台上。
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描述
产品名称:机载综合辐射监测系统
品牌:Nuvia
产地:法国
型号:AIRIS
机载综合辐射监测系统AIRIS算法提供对地面的观测数据重新计算、选定放射性核素的实时识别、飞机机组人员安全控制和智能飞行员调查指导。任务导航系统与飞行员引导单元 (PGU) 集成在一起。
数据采集系统提供内部数据同步和精确定位的实时计算程序。
机载综合辐射监测系统AIRIS带有数据采集软件的坚固笔记本电脑允许操作员控制所有测量参数、实时光谱和剂量率、地图视图导航、警报等。
能量范围: 30kev – 3MeV
范围: 5nGy/h – 0.1Gy/h(使用 GM)
探测器: 四个 4 升(=16 升)NaI(Tl) 伽马探测器
中文内容来自机器翻译,内容仅供参考,实际内容可参考原厂介绍或以合同为准。
英文原文:
AIRIS
Airborne Integrated Radiation Information System
AIRIS is designed for airborne radiation measurement based on gamma spectroscopy. The system can be installed on fixed-wing and helicopter platforms.
The algorithms provide observed data recalculation to the ground level, real-time identification of selected radionuclides, control of aircraft crew safety and intelligent pilot survey guidance. The mission navigation system is integrated with a Pilot Guidance Unit (PGU).
The data acquisition system provides internal data synchronization and real-time calculation procedures with precise positioning.
A rugged laptop with Data Acquisition SW allows the operator to control all survey parameters, real-time spectra and dose rate, map-view navigation, alarms and others.
E-Resolution: <8.5%@662keV
Energy range: 30kev – 3MeV
Range: 5nGy/h – 0.1Gy/h (with GM)
Detectors: Four 4 Litre (=16 Litres) NaI(Tl) gamma detectors
品牌:Nuvia
产地:法国
型号:AIRIS
机载综合辐射监测系统AIRIS介绍:
AIRIS 专为基于伽马光谱的机载辐射测量而设计。该系统可以安装在固定翼和直升机平台上。机载综合辐射监测系统AIRIS算法提供对地面的观测数据重新计算、选定放射性核素的实时识别、飞机机组人员安全控制和智能飞行员调查指导。任务导航系统与飞行员引导单元 (PGU) 集成在一起。
数据采集系统提供内部数据同步和精确定位的实时计算程序。
机载综合辐射监测系统AIRIS带有数据采集软件的坚固笔记本电脑允许操作员控制所有测量参数、实时光谱和剂量率、地图视图导航、警报等。
机载综合辐射监测系统AIRIS参数:
电子分辨率: <8.5%@662keV能量范围: 30kev – 3MeV
范围: 5nGy/h – 0.1Gy/h(使用 GM)
探测器: 四个 4 升(=16 升)NaI(Tl) 伽马探测器
中文内容来自机器翻译,内容仅供参考,实际内容可参考原厂介绍或以合同为准。
英文原文:
AIRIS
Airborne Integrated Radiation Information System
AIRIS is designed for airborne radiation measurement based on gamma spectroscopy. The system can be installed on fixed-wing and helicopter platforms.
The algorithms provide observed data recalculation to the ground level, real-time identification of selected radionuclides, control of aircraft crew safety and intelligent pilot survey guidance. The mission navigation system is integrated with a Pilot Guidance Unit (PGU).
The data acquisition system provides internal data synchronization and real-time calculation procedures with precise positioning.
A rugged laptop with Data Acquisition SW allows the operator to control all survey parameters, real-time spectra and dose rate, map-view navigation, alarms and others.
E-Resolution: <8.5%@662keV
Energy range: 30kev – 3MeV
Range: 5nGy/h – 0.1Gy/h (with GM)
Detectors: Four 4 Litre (=16 Litres) NaI(Tl) gamma detectors
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