I am sorry for the late reply, antiterror13.
LoL
Firstly, I am definitely no expert.
My apology to all.
My earlier DF-5B posting was inaccurate.
According to this distant, indirect, unofficial and vague source ... ...
 Illustration of Hybrid rocket system
Illustration of Hybrid rocket system
 
 
The DF-5B is using a modular Hybrid rocket system of
( Liquid + Solid + Catalyst ) chemical fuels mixtures in all 5 flight stages.
The DF-5B uses special modular Liquid catalyst fuel tanks. 
Most parts are made using Additive Manufacturing method. 
Therefore they are at least 50% lighter and much more robust compare to DF-5A, 
and way faster and cheaper to produce, because the subtractive manufacturing 
( using CNC ) processes are less than 10%.   
The AM method also allow the production of highly precise 
( up to 20 microns accuracy ) Liquid fuel Turbopumps. 
Each DF-5B missile has a unique preset variable thrust during the downward 4th and 5th stages. 
Thus, each DF-5B missile flight speed is very unpredictable and leave no flight pattern. 
Using, modular Liquid catalyst fuel tank, ... ...
It only takes less than 3 minutes to fuel and launch. 
For comparison DF-5 can take up to 60 minutes to fuel and launch.
 
 
	
		
	
	
		
		
			Interesting, is there any other ICBMs with combination of solid fuel (1st stage) and liquid fuel ?
		
		
	 
Actually, Hybrid rocket system concept has been around since 1950. 
For example:  Virgin Galactic Spaceship 2 is using Hybrid rocket system. 
NOTE: 
Sorry for the secretive nature of ICBM, there is no link or website provided.
Please take this info with multiple grain of iodized salt. 
