
The Sanskrit alternates of Mangal are Bhaum and Angaraka.
Also, Mangal carries a mace, spear and trident while riding a ram. Perfect name and attitude onlee.
Saar apart from this, while naming LCH we should consider the non Hindi/Sanskrit speaking audience as well. After all, none will like some firangi pronouncing "Vyaghra" as "v*i*a*g*r*a" though it's a very good name. JMT.uddu wrote:The only criteria must be that name must not be a fancy name but must really create fear in the minds of the enemy during war.
Narayana Rao wrote:looks like a camachi to me
http://livefist.blogspot.com/2007/05/ca ... -more.htmlI do have an answer about the port offset canopy. The first Canberras were built with the "goldfish bowl" canopy. The pilot sat to the left and there was a walkway to his right that the navigator used to walk to the nose bomb aimer position. While not over the target the navigator sat in the seat behind the pilot.
Then the Canberra was modified for the low level attack role - this was the major variant that the IAF ordered (the B.58)
The British wanted to make it a "minimum change" variant and needed better visibility for the pilot. So they left the pilot position where it was (ie. on the left when looking out from the aircraft) and put a bubble canopy over it. That resulted in the lopsided offset canopy look. The Brits also did this for the Sea Vixen aircraft.
This resulted in the navigator not having an ejection seat in the B.58 variant. The US modified their Canberras with a proper front and back seat, not taking short cuts.
These criticisms are pretty harsh. Are they accurate?The fact that India cannot fight wars lasting more than 10-15 days is not an accident, but a deliberate policy choice which, incidentally, is mirrored on the Pakistani side as well. The Indian armed forces can use their budgetary allocations to build up their capacity to fight long duration wars by filling what are called "voids" -- the unmet requirements of war material -- the maintenance spares and stores, ammunition and shells and reserves of petroleum, oil, lubricants (POL). Instead, they choose to invest in new weapons platforms -- tanks, guns, aircraft, and ships-- to keep the Indian military technologically up to date. Further, the largest quantum of capital defense spending (26 to 32%) continues to be on armor, a combat arm with a great history but dim future, with a good part of these funds tasked for replacing a good main battle tank (T-72S) in service with a still newer MBT (T-90), with other mission capabilities suffering neglect. However, there is no matching concern for augmenting stocks of spares and shells for tank guns, etc. In 1993-94, the "voids" requirements of spares , POL, and ammunition and shells for armor and artillery for the army amounted to some $100 billion (Rs 42,000 crore), which figure currently has, perhaps, crossed the $300 billion (Rs 120,000 crore) mark. Because newer MBTs are more and more expensive, progressively fewer of the latest tanks are inducted into the armored formations, and even larger numbers of the older tanks are decommissioned or mothballed. Unbalanced defense expenditure means there is, for instance, no worthwhile capability for offensive actions on the Tibetan plateau against China and considering, its prime maritime location, relatively meager sea denial and sea-control assets (both these missions now consume only around 15% of the defense budget.). Similar strategic myopia has has eventuated in the Indian Air Force's having great aerospace pretensions but, owing to its preference for short-to-medium range fighter aircraft that fills its inventory, no strategic reach.
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Where Cold Start is concerned, there may be three strike corps available for offensive operations. In reality, there is combat hardware and spare sufficiency to equip and operate only one strike corps at full tilt at any given time -- the showpiece II Corps.
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For rapid advance of armor, Cold Start relies on combat aircraft to clear the path. ... However, close air support is a role the Indian Air Force is not enthused about and does not plan or train its pilots for.
I didn't get you. ALCMs like the Kh-59, JSOW et al are technically BVR ATG missiles.Mayuresh wrote:Guys, a newbie question.
How feasible is it to make a BVR ATG guided missile/bomb? I have never heard of any such thing before.
I think you are right. I was thinking more on the lines of a typical A2A BVR missile where the a/c locks on to a target and then guides the missile to it. Cruise missiles (say a BrahMos launched from our Rambha) would probably still be guided by GPS or some other means and would have its target pre-decided and co-ordinates fed even before the missile is loaded.nachiket wrote:I didn't get you. ALCMs like the Kh-59, JSOW et al are technically BVR ATG missiles.
A standard Paveway type LGB is exactly such a munition. In Kargil they were released at 8.5 km away from the target - which is, strictly speaking, BVR.nachiket wrote:I didn't get you. ALCMs like the Kh-59, JSOW et al are technically BVR ATG missiles.Mayuresh wrote:Guys, a newbie question.
How feasible is it to make a BVR ATG guided missile/bomb? I have never heard of any such thing before.
This first ever fixed wing aircraft landing at Nyoma, the army’s newest Advanced Landing Ground (ALG), close to the frontline with China, was made possible by a new “miracle compound” called RBI-81
We need this is huge quantities...The 2.7-kilometre airstrip was built in just 90 days by jawans who had never worked with RBI-81. All they had to do was to mix RBI-81 with local mud, sprinkle water over the surface and then run a road roller over the mixture. Hardening instantly, the surface easily withstands repeated landings by the 20-tonne An-32.
During Kargil, the IAF reportedly did things to some of its Mirage-2000s that would have amounted to serious violations of the Indian government's contract with Dassault. It is understood, but not confirmed, that the French government was quietly engaged after the war and the two sides were able to agree that it was not a problem, and that no penalties would be slapped on the Indian government for what were, in reality, war exegencies, even though it was clear that there had been serious breaches of the technology agreement.
I believe what the article is referring to is what we did with the Mirages, integration of Litening LDPs and the employemnt of LGBs to hit the high altitude targets. The Yehudis helped out in this regard and the Litenings were wired up very quickly. Thats all I know.AdityaM wrote:can someone throw more light
http://livefist.blogspot.com/2010/08/wh ... icans.htmlDuring Kargil, the IAF reportedly did things to some of its Mirage-2000s that would have amounted to serious violations of the Indian government's contract with Dassault. It is understood, but not confirmed, that the French government was quietly engaged after the war and the two sides were able to agree that it was not a problem, and that no penalties would be slapped on the Indian government for what were, in reality, war exegencies, even though it was clear that there had been serious breaches of the technology agreement.
Won't any Naval fighter (heavy or non heavy) that operates from STOBAR aircraft carriers be able to operate from such a facility? The Su-33 uses a ski-jump to operate from Admiral Kuznetsov, so I don't see any problems why they would not be able to operate in the mountainous regions. I am guessing the concern would be around the air density in the mountains being lower than that at sea-level, so a larger STOBAR setting required than on a carrier, but then that would be true for conventional airfields too.Gaur wrote:^^
That would mean that only non heavy Naval fighters with very good t/w ratio (or the likes of sea harriers) can be operated. Also, the IAF pilots would have to given specific training regarding that.
Well, having four or five STOBAR runways each on airfields near the border would definitely benefit the resistance to Cruise missiles and other likelihoods.Is there so acute shortage of space near border (or in mountains for that matter) that we need to resort to build specialized runways. If so, I have not heard of such. However, more knowledgeable members can contribute more in this matter. Also, how many airbases are required right on top of high mountains?
Even though they might cost more, if we have the air platforms capable of using them in place, the benefit they offer during emergencies even for a short period could be valuable.Would the STOBAR runways cost more or less? More is my guess.
Ok I will take it that I goofed up on Test-pilot ejection at extremes of envelope part and my apologies to all pilots. But how technically challenging it is to program an auto-pilot into doing the same, that is - repeating a specific manouever with incrementally increased aggressiveness ? And doing this over an uninhabited area like the ocean airspace.Gaur wrote:I do not mean to sound condescending but I am seriously finding it difficult how one can suggest these ideas? Was this supposed to be a joke?
That would still be positive news isn’t it?Gaur wrote:If ADA were to announce that they were doing an intentional "destructive testing", what will ADA do if all goes well during the tests and the a/c does not suffer any malfunctions? Crash the aircraft anyways? Do you have any idea regarding the time and effort to build a new prototype?
Nope, referring to the overengineering bit that comes from a greater engineering factor of safety. There is a material thickness that is determined by engineering to withstand all the stresses you mention but there is extra material provided due to higher than usual factor of safety. An established aerospace major would need to use a lower factor of safety. Accelerated fatigue testing on ground till actual failure of shaved prototypes could be conducted.Gaur wrote:The aircraft is over engineered because it has to withstand the stress of being flown for thousands of hrs over the period of 30-40 years. Sure, you can shave of 1000kgs and flow it for number of tests and maybe nothing would go wrong. But what guarantee would you have that the aircraft would be able to withstand the stress after even one decade.
The soviets dropped tanks with parachute didn’t they? But I take it I messed up on that part. But the idea was not to save the prototype intact since it is a destructive test but to retain specimen with ONLY the fractures that happened due to extreme manouevers for subsequent study. Not to have new fractures and breakages from crashed landing of the specimen.Gaur wrote:And you want to use parachute on a 5700 kg aircraft nosediving at supersonic speeds or perhaps facing a spin? Well, good luck with that.
8 planes / year and start counting the time we spent testing Tejas(since first prototype) and intend to continue spendingGaur wrote: Do you have any idea regarding the time and effort to build a new prototype?
INSAS AR uses NATO standard 5.56x45 mm. cartridges, as do most western ARs. Complaints about the 5.56x45 mm. caliber's lethality are nothing new. There is a tradeoff that designers must make between caliber and weight of each bullet vs. how much ammo a soldier can carry and controllability of the weapon.Carl_T wrote:On one thread where an interview with IA soldier was posted, I read that the Insas wasn't "lethal" enough and they desired I think a rifle with a bigger caliber. Question though - don't most ARs use pretty standard cartridges?
Thanks in advance.
If you have further queries, I suggest you ask Kartik. Unlike me, has the expertise in this area. So, he will be able to provide better answers. I have written all that I know regarding the subject and find myself repeating the same things I said in my earlier post.Shiv wrote:After a crash it is impossible to tell exactly which part of which component failed - i.e to reconstruct the cause of the crash So a destructive test may fail to give any info.