Fig. 1 Rotor Disk Clearance in MIL-STD-1289D
Fig. 2 Flow Field at Hover, Modeled with Peter-He 15 State Dynamic Inflow Method
Fig. 3 Flow Field at Hover, Modeled with Prescribed Vortex Wake Method
Fig. 4 Hydra70 Rocket Configuration
Fig. 5 Hydra 70 Rocket Thrust
그림 6 Rocket Installed Position
Fig. 8 Flow Chart of Rocket Launch Analysis
Fig. 9 Downwash Velocity along the Flight Path of the Rocket
Fig. 10 Rocket Pitch along Flight Path of Rocket
Fig. 11 Effect of Main Rotor Interference on Rocket Trajectory
Fig. 12 Main Rotor Disk Clearance
Fig. 13 Launch in Forward Flight Maneuver
Fig. 14 Launch in Rearward Flight Maneuver
Fig. 15 Unsafe Rocket Launch Envelop in Vertical Climb Maneuver
Fig. 16 Downwash Velocity in Vertical Climb Maneuver
Fig. 17 Rocket Pitch Angle in Vertical Climb Maneuver
Fig. 18 Unsafe Rocket Launch Envelop in Forward Climb Maneuver
Fig. 7 The Validation of Rotor Induced Flow Distribution at Rocket Pod Waterline level
Table 2 Rocket Mass and Configuration
References
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