
-Vivek
Looks like a raging bull heading for the matador.narayana wrote: Shourya Picture 1
I've my doubts that the chromium research would provide deployable technology within a few months of it being announced.Philip wrote:..and add to the range the extra distance if the missile is coated with the latest "chromium" paint that allegedly doubles the range of any missile coated with it due to reduced drag.The interesting detail is the diameter of the missile (half a metre).This is a very compact dimension and could see a large number of missiles aboard out future subs.
Rahul, check the diameter difference between the Agni-1 and K-15 missiles. The K-15 is a lot thinner and compact. I am guessing it has a lot to do with the advancement in materials technology since the days of Agni-1 design work that allows for such changes. So now you have a missile that is much more compact and therefore easier to handle but with roughly the same range. But having said that, the Agni-1 would still be needed to bridge the gap between Agni-2 and Shaurya series etc.Rahul M wrote:I wonder what was the need to replace the Agni-1 type, more range perhaps ?
The hydrodynamic thruster cap surely means that this missile has been designed for underwater launch. But what is that pink exhaust emanating from the top of the booster (?). Is it a leaking booster?narayana wrote:Shourya Picture 1
The chromium vapour drag reduction comes into play during reentry and the nose of this missile has a typical aero spike for drag reduction.Brando wrote:I think one can also see the whole "chromium vapor" drag reduction thing they were talking about with the nose cone on the second picture.
I guess the Defence guys have really started to read Vivek's scenerios. Keep up the good job Vivek and write some more scary chinki stuff. It will surely help the speedy induction of Nirbhay.The sophisticated tactical missile is capable of carrying conventional warheads with a payload of about one tonne.
Hmm, is it cold launch? I don't see any 'flame/Exhaust' inside the launch tube.arun wrote:Photo of the Shourya from the PIB website :
Shourya Pic
Guess this is national property and thus free to use.
Brando wrote:I doubt the "Shourya" missile is a "surface to surface" missile as the Press Release claims. The whole things looks like it was meant as a SLBM with its toned down size and its ejecting nose cap and the weird rocket motor attachment at the base. They probably just wanted to test the missile in air to see if all the mechanisms worked fine and in the proper order before an underwater test.
yes, me too curious.Austin wrote:So if this is not the K-15 Sagarika SLBM , is this a new system for the army .?
shetty wrote:On the news I heard them say that this will replace the Prithvi. 250 - 350 km vs 600 km ??? Doesn't make sense. Some explanation required.
The flow spike is not typical for a ballistic missile. The chromium vapor drag reduction theory essentially says that the chromium is vaporized due to the frictional drag and creates a new boundary layer over the nose cone of missile. Its not dependent on atmospheric friction of re-entry.neerajbhandari wrote:The chromium vapour drag reduction comes into play during reentry and the nose of this missile has a typical aero spike for drag reduction.Brando wrote:I think one can also see the whole "chromium vapor" drag reduction thing they were talking about with the nose cone on the second picture.
Cheers....
Developing a cutting edge SAM is not easy, and when it comes to naval based options one needs some really advanced radars, I mean whats the use of a P15A with not-so-good radars? Do we have a single working AESA radar yet?Avarachan wrote:I've always been puzzled by the need for this co-development of the MRSAM with Israel ... It seems quite expensive, and it would seem that between the Akash and the AAD, we have enough indigenous expertise to develop a missile like this on our own. Can any of the gurus shed some light on this? I remember that when this co-development was announced, JCage was puzzled about it, too.
no saar ji, brahmos is liquid fuelled CM, this is solid fuelled BM.Anurag, Is this an upsized Brhamos? The bottom is a solid booster that separates. The payload is one tonne vs 300kg. All else looks similar.
A number of Russian SLBMs do this.ramana wrote:Interesting way to get the ballistic cap off!
SaiK wrote:I would think of lesser drag tech nosejob use for escaping gravity, and preserve the fuel for midcourse+ .. and voila!~ we could potentially be converting A3->S1.
+correction.