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ONBOARD INSTRUMENTATION FOR SCRAMJET ENGINE FLIGHT TEST

机译:SCRAMJET发动机飞行测试的车载仪表

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This paper brings out the design details o f an instrumentation system that was used in ISRO fs recent Sc ramjet Flight Test.The successful demonstration of supersonic combustion and evaluation o f scramjet engine performance thrust were monitored through a number of pressure,temperature and acceleration parameters.The instrumentation subsystems for performing this function were distributed in the scramjet engine and the upper payload bay.This paper describe the design,qualification and performance char act erizcition o f the instrumentation and base band telemetry system with specific focus on those measurements which are critical for assessing the success of the mission.
机译:本文介绍了ISRO最近进行的超冲压发动机飞行试验中所使用的仪表系统的设计细节。通过许多压力,温度和加速度参数监控超音速燃烧的成功演示和超燃发动机性能推力的评估。用于执行此功能的仪器子系统分布在超燃冲压发动机和上部有效载荷舱中。本文描述了仪器和基带遥测系统的设计,鉴定和性能特征,特别关注那些对评估性能至关重要的测量。任务成功。

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