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To achieve outside atmospheric kill and it destroys incoming Warhead by its shear kinetic energy. Tube like structures are there to control KKV in the space and mode of work is similar to Reaction control system.

@Dillinger: It is kinetic kill vehicle. AFAIK,ISRO was incharge of developing KKV for DRDO.KKV is generally there is all exoatmospheric inteceptors and ASAT missiles.

Is it a KKV.?

@Dillinger: he-man ke bare me bol rahe ho.? Question pe question sigh...!

What's your RMR.? Mine is around 1400

@Dillinger: I had 17.9 BMI 3 months ago and now it is 19.1.So in 3 months ma body has changed from underweight to normalweight category. I used to think that my will remian thin no matter how hard i eat.But the thing is that our body has higher metabolism rate than rest of other,that's why our...

Kya hoga.? Jyada se jyada sugar,heart problems hoga.:rofl:

@Dillinger:Bro I need to goto gym .Gonna reply/chat with you tonight.Bye.

Yes i think you're right about wing loading of 2nd hardpoint.LCA is draggy in its current stats(As per some TT),so it might well increase drag issue. If the drag issue is solved then we might see multi-ejector racks in MK1/2 it'll A great a way to increase hardpoints but a bad way to increase...

In December.

@Dillinger: But sometimes I wonder why IAF wants Fly-by-light FCS.FBW FCS is good enough for atleast 2 decades.F-22,F-35,J-XX all have FBW.Though production variant of ATD-X will have FBL,but again nippos are ahead of us in this field. IIRC,HAL has developed Fly by light rotor control system...

Since Scramjet engines only work in around 4-5 mach numbers,It is generally developed with turbofan+ramjet engine to remove the need of Solid rocket boosters. So basically Hypersonic space plane will have:1)Turbofan:for horizontal takeoff.Then after attaining M2 speed engine will be switched...

Frim what i have read from the souvneir.They'll 1st develope DMRJ then after mastering it they'll integrate DMRJ for Hypersonic test vehicile(HTV). 1)It would take-off horizontally using conventional turbo-rocket.After it has reached cruise speed of mach 1-1.2, vehicle would use DMRJ dual mode...

Brahmos-2 with 300KM is very much feasible if combustor can sustain around 60 sec burntime(D=By booster+scramjet). ISROs version is a bit different though.Ramjet+scramjet both coupled in one engine=DMRJ.

Sustaining 12 minutes scramjet propulsion will be challenge,but'll be worth taking.X-51A can sustain supersonic combustion inside its combustor for around5 minutes,that's 300 sec.

Hopefully.Scramjet technology may help Brahmos-2. It looks like they have finaly broke 20 seconds envelope.:cheers:

One is for Civilian space use while later will be used for future longrange 1500km cruise missiles.DRDLs scramjet project has been ground tested for around 7 seconds. An interesting paper by DRDLs director about our scramjet project...

@Dillinger: No idea,but it may take atleast 1 year after they have ground tested combustor for 7 seconds. DRDLs Scramjet project is current leading now,with its flight in 2014.

Wrong thread bro.wrong thread.