. Airborne radar. Airplanes; Guided missiles. Fig. 10-10-a A Typical Transonic Radome Resting on the Concrete Apron in Front of the F4D Aircraft, Showing the Fire-Control Radar and Antenna Exposed in the Nose .0 MACH NUMBER Fig. 10-10-b Temperatures Expected at the Tip of a Missile Radome as Function of Velocity and Altitude. however, in an easing of the electrical requirements. With a proportional navigation system such as is often used in missile guidance, the actual bore- sight error is not of consequence compared with the rate of change of apparent error with respect
. Airborne radar. Airplanes; Guided missiles. Fig. 10-10-a A Typical Transonic Radome Resting on the Concrete Apron in Front of the F4D Aircraft, Showing the Fire-Control Radar and Antenna Exposed in the Nose .0 MACH NUMBER Fig. 10-10-b Temperatures Expected at the Tip of a Missile Radome as Function of Velocity and Altitude. however, in an easing of the electrical requirements. With a proportional navigation system such as is often used in missile guidance, the actual bore- sight error is not of consequence compared with the rate of change of apparent error with respect to angle.'** Practical limits for this rate of change of radome error are nearly ±° per degree. ^^The Radome Problem in Guided Missiles, Final Report, N60NR27023. March 1, 1952, Princeton Please note that these images are extracted from scanned page images that may have been digitally enhanced for readability - coloration and appearance of these illustrations may not perfectly resemble the original Povejsil, Donald J. Princeton, N. J. , Van Nostrand
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Keywords: ., bookcentury1900, bookcollectionbiodiversit, booksubjectairplanes
