This report describes the instrumentation provided for D Series IOC Missiles. The measurements listed in the report were selected and coordinated to provide gross malfunction data. The purpose of the report is to familiarize personnel with the airborne instrumentation and the general characteristics of the IRSS telemeter. The airborne data system is an PAM/FM/FM telemeter using an RF carrier which, as well as being modulated with information indicating gross performance of the missile also serves as an RF signal stimulus for two AME Cotar ground stations. The Cotar systems provide a 'real time' tracking input to the range safety system. Gross malfunction data is obtained from a small group of propulsion, autopilot, guidance and supporting systems parameters. (Author)
WS107-Ainstrumentation Configuration of Ioc Missiles-Irss
1958
46 pages
Report
No indication
English
Common Carrier & Satellite , Missile Technology , Surface to surface missiles , Telemeter systems , Instrumentation , Failure , Pressurization , Propellant control , Inertial guidance , Guided missile ranges , Guided missile tracking systems , Real time , Automatic pilots , Ground support equipment , Command and control systems , Nose cones , Guided missile components , Guided missile safety , Destructors , Pneumatic devices , Hydraulic equipment , Combustion chambers , Booster rockets , Sustainer engines , Vernier rocket engines , Gyroscopes , Pitch(Motion) , Yaw , Roll , Atlas , Xsm-65d missiles
Development of a Tactical Helicopter Infrared Signature Suppression (IRSS) System
British Library Conference Proceedings | 1997
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