Most Ballistic missiles generally leave the atmosphere and reentry. Hypersonic missiles do not have to leave the
atmosphere this makes them hard to detect and deflect. Brahmos is a ramjet cruise missile the next generation Brahmos
will be scramjet based? Then there is shourya and the K missiles which are in a class by itself.
I never questioned the advantage of hypersonic missiles. The big problem here is cost and labour to manufacture them. The range is also short. So, launchers have to be close to borders and we can only use it on Pakistan.
Ballistic missiles, on the other hand, are extremely cheap and easy to manufacture. For every Hypersonic missile made, one can make 5 ballistic missile of same range. I will give an example of cost of supersonic missile - Brahmos. It is 2.7 million dollars per missile. It may become less if seeker and motor is made in India, but even without them (60% of cost), it is still costly. I can only imagine how much Hypersonic ones may cost.
If in any war, missiles are used, one can expect it to escalate and hence nucleae war may be inevitable.
Noob questions..apologies to digress from topic at hand....since ASAT capability was discussed in this thread...
An ASAT scenario envisages the following:-target acquisition - flight to target- target destruction
We can modify on short notice existing space vehicles as kill vehicles...but what about target acquisition capability? Do we have powerful radars for dat? For acquisition, guidance n lock? Sats in GEO travel at roughly 3kms/sec at an altitude of 36000 Kms....sats in LEO travel at roughly 7kms/sec at an altitude of upto 2000kms...dat s in a second the sat would be 7kms away from its original position. We do have midway guidance capability but wat about acquisition n lock part of such high speed target
What about the warhead to be used.. there r hundreds of sats out there of different nations...wat type of warheads r used to minimise debris field..it has to be kinetic kill n not a proximity kill? to reduce collateral damage to other countries satellites...impact fuse is used in AAM, is the same thing used?
Flight to target capability is amply demonstrated by PSLV/GSLV...but is it accurate enough for kinetic kill? (Presuming preferred type of kill is kinetic). We know that sat positioning of PSLV/GSLV have a built in error margin of few hundred meters...dats one reason dey use the satellite's motors to navigate to required accurate position after ejection from payload fairing.(one of the GSLV launch with russian cryo engine had also fell short of target altitude by a large, though managable margin of 1000kms)
During cold war USA/Russia war gamed ASAT capability using AAM on specially modified jets to get to the edge of space n use radar to guide the missile to satellite.
In GEO, satellites are orbiting in the same speed as earths rotation and hence the speed is canceled out. One can be sure in geostationary orbit, at which point above earth the satellite is located. It will be very easy to destroy it. In geosynchronous orbit, the satellite makes a predictable path with the same speed as earth's rotation, but not around equator as circumference. So, that too can be traced easily. Geosynchronous satellite reaches exact same spot as previous day at a certain point of time.
In LEO, the orbit is still predecided but not as easy as GEO. In LEO, orbits of satellite have a certain perigee and apogee, are elliptical in nature. But, even then after observing for a few hours or days, it can be predicted. So, even it is very simple to strike satellites as the missile already knows before it launches where exactly to hit.