“The HF-3 missile uses a rocket-ramjet propulsion system, with two side-by-side solid-propellant jettisonable strap-on rocket boosters for initial acceleration and a liquid-fueled ramjet (believed to be using JP-10 fuel) for sustained supersonic cruise. The missile features a wingless design with four strake intakes and four clipped delta control surfaces aft. The air intake design arrangement was reported to have been optimized for evasive maneuvering at terminal sea-skimming altitudes. The missile is designed to be capable of way-pointing and can be programmed to fly offset attack axes to saturate defenses. It is also capable of high-G lateral terminal “random weaving” maneuvers to evade close-in defenses.”>
http://www.peopleforum.cn/viewthread.php?tid=92611&extra=page%3D1
The basic platform and cruciform intake geometry must work well though, that missile had the navy peeing their pants over twenty years ago, wondering how to counter it.