aditya g
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K-15 asbm?................................
Description of arihant and details
Description of arihant and details
Looks like they dont want to annoy any except Pakis and Chinis therefore DRDO kept the range at bear minimum of 700 kms giving it impression of K15 test..........“Having an operational range of nearly 3,500 km, the missile was fired towards north for a shorter range. It covered more than 700 km before zeroing on the target with high accuracy reaching close to zero circular error probability (CEP),” informed the source.
this is interesting, as news have been coming in that 5-6 submarine ejection tests were carried out.INS Arihant had first successfully fired a prototype of K-15 (B-05) missile in November last year.
Can you provide a link for the minimum energy trajectory? A great development.All our SLBMs will henceforth will not be fired with Minimum energy trajectory but only with depressed trajectory .Congratulations to all the people who are involved in the K-series program development. Now if only they could provide us a pic of K-4 .
the deepest trenches available in the indian ocean like vema trench , chagos trench etclaunch zone will be in the
where on recieving command will rise upto 50m or so below water level to launch their payloadsthe deepest trenches available in the indian ocean like vema trench , chagos trench etc
Rule out porkies from here.Missiles flown on a depressed trajectory can have significantly shorter flight paths, and therefore significantly shorter flight times, than those flown on a standard trajectory of the same range.
me thinks this is porky specific for the time being given the reported ranges of around 3500km.
launch zone will be in the
this is handy for
1. clean cut nuclear 1st strike like taking out airbases with enemy aircraft's being primed with nukes and waiting to be launched
2. short time-of-flight (STOF) nuclear attacks on targets be it during 1st strike or 2nd strike
3. MOST IMPORTANTLY counter to porky tactical nukes , a missile fired in a depressed trajectory will reduce the reaction time of the porkis to retaliate as the flight time is much lesser and the missiles whose trajectory has been lofted re-enters with higher velocity and at steeper re-entry angles and hence lesser fight time from re-entry to impact compared to when launched in a minimum energy trajectory . near instantaneous retaliatory strikes will enable MAD to remain viable by enforcing measured graduated retaliatory nuclear response so that the porkis don't go all suicidal .
INDIA can counter porky blackmail by adopting or threatening to adopt a launch-on-warning policy easily enforceable on the ground by the STOF capabilities coupled with high accuracy of this missile.
porkies can bluff with tactical missiles, what India will do is raise the stakes , this will complicate things for porkies in many ways ,militarily to finance to international pressure etc .
they are facing pressure on tactical nukes we just keep piling up the pressure by the introduction of another complication.
in future application of these on longer range missiles will be able to spoof the BMD of china etc
basically a BMD Fire Control System observes the usual trajectory of a ballistic missile to identify it as a threat. Shaping the trajectory confuses the FCS and the threat might be ignored by it resulting in not firing the interceptors.
Where is that thread?? any link plsRule out porkies from here man. :biggrin2:
Their small tactical nukes are not even worth attention. :bounce:
INS Arihant is for power projection across the globe. Did you watch thread and news of American Security Concerns on Arihant? :biggrin2:
@warrior monkCan you provide a link for the minimum energy trajectory? A great development.
It is what I always suspected that missile ranges are greater than claimed. This means k4 missile range is also understated?
Usually depressed trajectory is to evade bmd
But in a naval launch would this be a factor?
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Reason is that their SATs could not detect our missile initially. :bounce:Where is that thread?? any link pls
You have to balance the variables in testing in depressed trajectory the lift and drag force , re-entry heating , burnout parameters etc Once the vehicle has reached its pre determined apogee which will be lower than minimum energy trajectory the RV (Re entry vehicle ) trajectory now depends upon gravity . Now there are two ways for depressing trajectory is to depress the trajectory early in boost phase by turning the missile through a larger angle . This difference in angle will be accentuated by the effect of gravity dependent bending the trajectories over the course of the flight this is known as symmetric . The other way is is to follow a standard MET trajectory until the missile reaches altitudes at which the atmosphere is rarefied then missile can then be turned to flatten the trajectory this is known as shaped trajectory. As far as K-15 is concerned it flied in a shaped trajectory like a hypersonic missile with apogee of 40 to 50 Kms extremely dangerous .@warrior monk
All well and good until we reach MIRV's, how does one test MIRV's in depressed trajectory.
Is that even tested with dummy warheads?
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