This missile is absolutely best in class. DRDO is an absolute master in solid propulsion. Thanks to @NeutronX, for pointing out something to me. I haven't read a single account in public space which correctly describes how it works. It's quite beautiful.

I used to think that maneuvering right after launch was achieved through differential thrust through those 4 nozzles. That's wrong. Actually, there are 32 small RCS motors fitted right behind those holes behind those nozzles.

Right after the missile is launched, it's speed is not high and the tail fins are not as effective. These 32 motors are used for maneuvering. Generally, these are used in march larger missiles and rockets. https://www.youtube.com/watch?v=mILewUS0wsU&ab_channel=SkyrootAerospace…

In the meanwhile, the main motor has "dual-thrust" profiles. During the boost phase, it generates 350 kgf of thrust. And at the sustain phase, it generates 100 kgf. I strongly believe that they have done so with the same motor. possibly using different grains and/or geometry.

This saves space and weight on a very small missile. And in the private space this can be produced in high numbers with good QC. I hope to see these not just in man-portable, but also on ground and airborne vehicles, especially Rudra and LCH

It also leaves the space for an even lighter and cheaper man-portable missile. DRDO did issue an RFP for such a missile a couple of years back. It was called MPDMS then. That would be in the Igla class. Let's see.