I don't think after making two variants of REK, RA'AD-I and II cruise missiles and H-2 and H-4 in house production it will be difficult for AWC to design new powered or glide SOW for JF-17.
It seems the main issue of RA'ÁD missiles are related to its air frame which in my opinion are
- Related to wide horizontal stabilisers at its rear section near exhaust
- Pop-out air intake at the bottom
So to make the RA'AD missile compatible with JF-17 redesign of these sections of air frame should do the job and in this case it is not like that we have to invent such solutions which were never think or used before, we have examples of
- X-type cross stabilisers against Horizontal stabiliser and
- Side Air intakes to turbojet engine
Examples of X-type cross stabilisers
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- Examples of Side Air intake
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other than this we should keep in mind that there is option of GB-6A cruise missile which is a version of GB-6 glide dispenser from China exist which if required can be used as stopgap solution ....
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