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Independent Orbiter Assessment (IOA): Analysis of the landing/deceleration subsystem [PDF]

open access: yes
The results of the Independent Orbiter Assessment (IOA) of the Failure Modes and Effects Analysis (FMEA) and Critical Items List (CIL) are presented. The IOA approach features a top-down analysis of the hardware to determine failure modes, criticality ...
Beaird, H. G.   +2 more
core   +1 more source

Structural Analysis of the Right Rear Lug of American Airlines Flight 587 [PDF]

open access: yes, 2006
A detailed finite element analysis of the right rear lug of the American Airlines Flight 587 - Airbus A300-600R was performed as part of the National Transportation Safety Board s failure investigation of the accident that occurred on November 12, 2001 ...
Davila, Carlos G.   +4 more
core   +1 more source

Independent Orbiter Assessment (IOA): Analysis of the orbiter main propulsion system [PDF]

open access: yes
The results of the Independent Orbiter Assessment (IOA) of the Failure Modes and Effects Analysis (FMEA) and Critical Items List (CIL) are presented. The IOA approach features a top-down analysis of the hardware to determine failure modes, criticality ...
Emmons, T. E.   +4 more
core   +1 more source

Advanced approaches to failure mode and effect analysis (FMEA) applications

open access: yesMetalurgija, 2015
The present paper explores advanced approaches to the FMEA method (Failure Mode and Effect Analysis) which take into account the costs associated with occurrence of failures during the manufacture of a product. Different approaches are demonstrated using
D. Vykydal   +3 more
doaj  

Independent Orbiter Assessment (IOA): Analysis of the ascent thrust vector control actuator subsystem [PDF]

open access: yes
The results of the Independent Orbiter Assessment (IOA) of the Failure Modes and Effects Analysis (FMEA) and Critical Items List (CIL) are presented. The IOA approach features a top-down analysis of the hardware to determine failure modes, criticality ...
Riccio, J. R., Wilson, R. E.
core   +1 more source

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