Pitot static system

Chakravarathy, R and Anupama, - (1992) Pitot static system. Project Report. National Aerospace Laboratories, Bangalore.

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The proposed pitot static system has two redundant channels. Each channel has a pitot static tube having two static ports and one pitot tube. The altimeter and vertical speed indicator are connected to one of the static ports of both the systems. The airspeed indicator and airdata computer are connected to the P and S ports of both systems. This method of connecting the pitot static system to the service improves the system servicability with adequate redundancy.

Item Type: Monograph (Project Report)
Uncontrolled Keywords: Pitot static tube;Air data system
Subjects: AERONAUTICS > Aircraft Design, Testing & Performance
Depositing User: Smt Bhagya Rekha KA
Date Deposited: 21 Jan 2013 04:29
Last Modified: 21 Jan 2013 04:29
URI: http://nal-ir.nal.res.in/id/eprint/11444

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