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Figure 1 X-15/BLUE SCOUT LAUNCH SYSTEM |
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Figure 2 PROFILE OF PACIFIC MISSILE RANGE LAUNCH |
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Figure 3 PROFILE OF ATLANTIC MISSILE RANGE LAUNCH |
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Figure 4 NORTH AMERICAN X-15A-2 RESEARCH AIRCRAFT |
RAMJET SEPARATION CONDITIONS FLIGHT NO. 2-53-97 Velocity 980 fps Angle of attack 8° Altitude 35,500 feet Roll angle 57° left Mach Number 0.98 Normal accel. 1.6 g Dynamic Pressure 340 psf |
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Figure 5 THE PROPOSED DELTA-WING X-15, NOVEMBER 1964 |
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