System Flight control Aero 3 Air vehicle functionality Integration Lab system simulation (mission, range, takeoff, testing components & with landing, air worthiness) with X X software damaged damaged FCS components systems & and/or FCS surfaces surfaces 1.2.1.3.x VULNERABILITY OF AIR VEHICLE TO PROPULSION SYSTEM THREAT INDUCED DAMAGE (Ballistic & Fire) FASTGEN/ UEDDAM Used engine COVART/ X, C-130J 1 Engines X (If warranted FMECA/ prop data by Pk analysis) DMEA Pk analysis FASTGEN/ COVART/ 2 Engine Nacelles including X Surrogate FMECA/ fuel & hydraulic lines DMEA Pk analysis 3 What is the functionality Engineering Prior combat and (mission completion, range, analyses flight commercial takeoff & landing, air simulation incident data worthiness) of the air vehicle with damaged or inoperable propulsion systems (engines, propellers, nacelles)? 1.2.1.4.x VULNERABILITY OF AIR VEHICLE TO AVIONICS/ELECTRONIC SYSTEMS THREAT INDUCED DAMAGE 1 What is the vulnerability FASTGEN/ (redundancy, separation) of COVART/ mission/flight critical FMECA/ avionics/electronic systems to DMEA Pk expected ballistic threats? analysis
3 Air vehicle functionality (mission, range, takeoff, landing, air worthiness) with damaged FCS components and/or FCS surfaces System Integration Lab testing Flight control system components & software X Aero simulation with damaged systems & surfaces X 1.2.1.3.x VULNERABILITY OF AIR VEHICLE TO PROPULSION SYSTEM THREAT INDUCED DAMAGE (Ballistic & Fire) 1 Engines X Used engine (If warranted by Pk analysis) FASTGEN/ COVART/ FMECA/ DMEA Pk analysis UEDDAM X, C-130J prop data 2 Engine Nacelles including fuel & hydraulic lines X Surrogate FASTGEN/ COVART/ FMECA/ DMEA Pk analysis 3 What is the functionality (mission completion, range, takeoff & landing, air worthiness) of the air vehicle with damaged or inoperable propulsion systems (engines, propellers, nacelles)? Engineering analyses flight simulation Prior combat and commercial incident data 1.2.1.4.x VULNERABILITY OF AIR VEHICLE TO AVIONICS/ELECTRONIC SYSTEMS THREAT INDUCED DAMAGE 1 What is the vulnerability (redundancy, separation) of mission/flight critical avionics/electronic systems to expected ballistic threats? FASTGEN/ COVART/ FMECA/ DMEA Pk analysis
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