Based on the aerodynamic heating simulated results of a spinel middle-infrared (Mid IR) image
guide missile dome flying at supersonic speed, a series of experiments are made and some methods of
eliminating aero-heating effect are carried out successfully. First, a simulation experiment on the
ground discarding an outside protective shell of a spinel dome is accomplished in order to inspect the
withstanding impact ability of the dome. Second, an arc wind tunnel experiment is fulfilled to obtain
thermal mechanics characteristic of the spinel dome, and a method to buildup obviously mechanics
intensity is approved which is coating diamond protective layer on the external wall of the spinel dome.
Third, two heated dome imaging experiments on the ground are made to study the aero-optical
phenomenon. Finally, a rocket sled experiment of a guide missile head is made successfully.
Experimental results show that when the guide missile head flies in a supersonic, by adjusting the
frame integration time of detector etc. the aero-optic effect would decrease greatly.
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