India did not enter the "hypersonic missile" group with this missile.
And that thing on the nose is an anomaly, not a feature.
Here's a quick and dirty thread on where this missile lies on the technology spectrum and what it means to India's security.
The easy thing first. That disc at the top is just the cover of the canister. It's supposed to rupture at launch, but it did not. It got lodged in the nose and was broken only due to aerodynamic forces as the missile achieved speed.
Undesirable, but solvable.
Now, let's come to hypersonic missiles. Hypersonic missiles are any missile that's flying above Mach 5. All missiles from the Agni series do so. All missiles from K-series also do so.
Let's first understand what is happening here. As you studied in high school, to throw a stone far away you must throw it at 45 degrees to the horizontal and throw it is as hard as you can.
The closer you are to 45 degrees, and the faster you throw, the further the stone goes.
That's called a minimum energy ballistic trajectory. shown by the black line here. That's fine and dandy as long as we don't take three things into account.
1. inaccuracies of manufacturing of the missile, 2. atmosphere, and 3. the chances of interception
Because of the first 2 aspects, inaccuracy and atmospheric interference, your projectile will deviate from its target. This deviation is typically a fraction of the range. But at thousands of kms range, you will miss your target by kms even with the slightest of deviations.
So, you need some kind of trajectory correction once you reenter. This is what you see in MARV warheads on Agni-2 and Agni-1P.
Think of them as a badminton shuttle cock. The fins are used mostly to correct for error.
Graphics by somebody else.
With these corrections, you can change your error from a few kms to a few 100s of mtrs in Agni2's case and to few 10s of mtrs in Agni 1P's case.
They can also maneuver the reentry vehicle to a certain extent to evade interception.
In the case of the Agni series, the enemy can see the approaching warhead for minutes. If they have a modern ABM, it can identify the best interception point and path in a few seconds.
But the MARV warheads will maneuver itself just enough to make that interception point invalid
So MARV is a hypersonic re-entry vehicle which maneuvers to increase precision and avoid interception. And India got there in the early 2000s.
But India went a step forward with the K-15 missile and its derivatives like Shaurya and Pralay.
The first thing that you must notice is that the while the fins of the Agni series are on the warhead, the fins of the K-15 derivatives or on the missile body.
This is because the missile body is retained at reentry to follow what DRDO calls quasi-ballistic trajectory.
In this quasi-ballistic trajectory or Boost-glide trajectory, the missile skips across the top of the atmosphere like a stone on a flat lake.
K-15 series uses its missile body to develop lift from the atmosphere to achieve this skip behaviour. Yes cylinders do generate lift.
This is better than MARV in 2 aspects. 1st, since the missile doesn't reach very high altitudes, it appears above the target horizon much later, decreasing response time significantly. Also, they can maneuver much more than an MARV thus further reducing chance of interception.
K-15's first test dates are shrouded in mystery but by the 2015, DRDO had mastered this tech. Many variants of K15 started arriving.
So what is this current missile?
While K15 series follows the skip glide trajectory, this missile follows the steady glide trajectory.
But why? Because they are intended to hit moving targets. Although the name is withheld, it is an open secret that it is designed to hit ships at 1500 km range.
This infographic is wrong, it is not a quasi-ballistic missile.
To hit a moving target like a ship, it has to 1 detect and track the ship and two hit it with extreme precision. If you miss a ship by 10 mtrs, nothing will happen to the ship!
One required CEP of <10 mtrs against a moving target at 1500 kms.
That's no joke!
You can't be skipping around at those speeds and hit a mobile target taking evasive maneuvers. You need to cruise, nice and smooth.
That's why this missile has wings. And don't think those wings are small. At those speeds they create very significant amounts of lift.
One can make many kind of gliders. DRDO has gone for the simplest one (relatively speaking). There are fancier hypersonic glide vehicles. They create lift more efficiently, but are more difficult to control.
Also, they would require fairings for boost phase.
I love DRDO's design because of its simplicity.
I am not clear of one thing. Is the glider powered during boost or after reentry. DRDO has several publications on low power solid rocket motors which would be perfect for the latter But I think this is not the case.
I think it is a 2 stage boosted missile. and it is a hypersonic guided glide vehicle at re-entry.
This brings us to the final. A frontier for mankind. Powered hypersonic glide vehicles.
DRDO's effort in this front is called HSTDV.
This kind of vehicle doesn't leave the atmosphere. It flies at constant hypersonic speeds by using scramjet powered flight.
ISRO and DRDO have both shown powered flight of a 6-20 seconds. But this is the ultimate frontier. And it's a challenge of all of mankind.
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Many things have changed since 2005, when the first 5th generation fighter F-22 was operationalized. Today's 4.5 generation fighters are technically superior to F22 in every aspect but stealth and thrust to weight ratio.
There so I am not going to use the term 4th generation and 5th generation. I am going to say stealth and non-stealth aircraft.
There is no bigger exponent of stealth aircraft than USA. and they have been very clear about their lessons.
Stealth aircraft are the tip of the spear. Because it is financially unviable to maintain a fleet of only stealth aircraft. So much so, that they are finding all kinds of adaptations for F22 and F35. "Stealthy pylons", "stealthy drop tanks". God knows what they mean!
Many of you want to know more about this locomotive.
This loco is completely designed and built by Chittaranjan Locomotives Works (CLW). This engine is an incremental development of the WAG9 engines which has been a workhorse for Indian Railways for the past two decades.
This is their 500th locomotive for the fiscal year. Their target is to produce 540 locos for this fiscal year.
If they manage do that, they will break their own world record of 436 that they reached last year. Year on year, this is a 24% jump in production rate.
There are many versions of the WAG-9 engines. These two engines belong to one of the latest called WAG-9Hi. The two engines combined produce 12240 HP.
This would make it slightly more “powerful” than the WAG-12B with 12069 HP. WAG-12B is produced by Alstom in Madhepura.
@TitaniumSV5 In this thread I will answer 3 basic questions: 1. Why does the first LM470 use 9 liquid methane-oxygen (methalox) engines? 2. Why develop new methalox engines, when ISRO is already developing semi-cryo kerosene-oxygen (keralox) engines for LVM 3? 3. Why 3 stages?
@TitaniumSV5 Q1. Why does the first stage of NGLV is going to have 9 engines.
Ans: The reason is actually quite generic. This magic number of 9 is common to a lot of modern launchers designed to: 1. Have a reusable booster, and /or 2. Have the same engine in the first and second stage.
1. Tejas Mk2 is happening 2. No major technical challenges 3. The rollout of Mk2 will predate AMCA/TEDBF 4. I wish the MRFA jamboree continues till Mk2 rollout because justifying it after Mk2 rollout and first flight will be very difficult.
I will just add my two cents about the questions being asked here.
This outrage/meltdown is good. This delay is a making of the decision makers, not engineers. So let them hear it.
Will they hear it? Does it matter? That's a different question altogether.
Orders for parts of the Mk2 have been placed.
Currently, no more delays are foreseen (there was never an engineering challenge).
If everything goes well rollout will be in 2025. First flight in 2026. (this is what I know. Take it FWIW)
This is an incredible footage of what is called a "hesitation roll". The aircraft flies nearly straight and level, rolling 90 degrees at a time and then 'hesitating' before rolling the next 90 degrees. The pass is completed with 4 such 90-degree rolls.
Here's a thread on ALH/LCH and LUH main gear box. The MGB is the magic around which the engineering is done. It is the primary reason behind ALH/LCH's phenomenal high-altitude performance.