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Hazards Analysis and Failure Modes and Effects Criticality Analysis (FMECA) of Four Concept Vehicle Propulsion Systems

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Figure

Figure 1:  Tilt-Wing Air Vehicle  1.4  Quad-Rotor Air Vehicle
Figure 2:  Quad-Rotor Air Vehicle  1.5  Side-by-Side (Lateral-Twin) Description
Table 1:  Mission Profile Summary of NASA RVLT Concept Vehicles  Passengers  Range  Type  Propulsion
Figure 5:  Proposed Vehicle Configuration Taxonomy.
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