amardeep mishra
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Ballistic missiles India has? Deployed,not under test.?
3 types of Liquid fuel Prithvi.
4 types Agni? out of which Agni 5 isn't deployed yet and Agni-1 status isn't sure if still in service or withdrawn and Agni 2 and Agni 4 are almost same with same design fired on lifted trajectory to increase range as Agni 4.
That leaves India with only 3 fat Prithvi with no multi launch capabilities as Prithvi is too fat and liquid fueled.
Prahar, Dhanush and K series not deployed yet.
And 3 types of Agni. Total 6 types of Ballistic missiles?
On the other hand Pakistan has Ghauri 1 and Ghauri 2. Then 4 types of shaheen and then Nasr,Abdali and Ghaznavi.
Total 7 types of Ballistic missiles deployed,considering Ghauri 1 and 2 same with different ranges.
Shaheen's status unknown if still deployed or withdrawn, but Shaheen-1, Shaheen-1A and Shaheen 2 deployed. Then Nasr,Abdali,Ghaznavi.
Total 7.
HI dear @shaheenmissile ..
I did not see your thread earlier,Now that i have read your thread,i would like to correct some of the factual discrepancies.Firstly all agni variants except A-5 are under production.A-4 was cleared for production this january- you can go through the official published literature of DRDO to confirm the information- no need to rely on wikipedia!
http://www.drdo.gov.in/drdo/pub/newsletter/2014/feb_14.pdf
and
here is the launch of A-4 in "deliverable configuration" conducted by none other than SFC.The misile has been cleared for production
http://www.drdo.gov.in/drdo/pub/newsletter/2014/december_14.pdf
Secondly i would like to comment on the completely erraneous statement regarding A-4. A-2 and A-4 are essentially two very different missiles.Have a look at the picture that i am attaching here-
AGNI-2
AGNI-4
As you can clearly notice some of the prominent features in A4 are-
1)There are no control surfaces in A-4 which means pitch and yaw corrections are obtained by TVC or gimballing the motor.Normally the deflection of motor rarely exceeds +/-8 degrees.and RCS(reaction control system) for roll corrections.
2)No truss structure separating the first and second stage.Instead shrouds have been used
3)Extensive usage of composites instead of maraging steel thereby allowing the missile to hit 4000kms with overall weight of 17tonnes!A-4 is infact smaller than A2 ,but weighs almost the same.In effect A-4 can do 4000kms whereas A2 is limited to 2500-3000kms.
4)Replacement of conventional gyroscopes and hydraulic actuators with MEMS based INS and actuators.
My dear, structural changes of aerial vehicles(be it missile or aircrafts) requires a lot of wind tunnel tests.For instance conventional missiles with external control surfaces use fin deflections to trim flight in a particular flight condition- either pitch,roll or yaw. The effect of fin deflection(de) on overall lift change(Cl) or in turn moment variation(Cm) is studied in wind tunnels.Whereas in case of modern missiles that dont have any external control surfaces,TVC is used to control pitching and yawing and RCS to control rolls. Control requirements are way more stringent in latter case. So when you do any structural modification ,you essentially have to pass your model through the wind tunnel and analyse aerodynamic data produced and then design the control systems for new configuration accordingly- which by no means is an easy task!
And lastly yes,dhanush is operationally deployed with IN.It was although a make shift arrangement by IN to have their own sea based nukes till K-series come online.
K-15 and K-4 have passed all the tests from pontoons and the firing of the missile from arihant would commence this year. Both of them are almost on the verge of getting inducted into the navy!
PS-Till now none of the pakistani missiles have #1,#2,#3 that i mentioned above
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