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Multiple-Target Missiles to redefine warfare

The A-5

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Precision-Guided Munitions
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S.K.Chaudari
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The technology demonstration of an ambitious
project to fire hi-tech precision-guided munitions (PGMs) from a mother
missile at various targets simultaneously will be completed in a year by scientists
of the Defence Research and Development Organisation (DRDO)
.
After technology demonstration, the first flight trial of a
200-km tactical missile to launch the PGMs is proposed to be carried out in two years
, according to S.K. Chaudhuri,
Director of Research Centre Imarat, a premier avionics systems hub of the
DRDO’s missile complex.

PGMs are miniaturised missiles with small seekers,
actuators and on-board computers and will be integrated with tactical missiles
having a range of 100-200 km
. The major
advantage of PGMs is that collateral damage could be avoided while attacking
multiple targets in a war scenario with sub-metre accuracy
.

Observing that the technology of a mother missile launching PGMs was a
frontier area, Dr. Chaudhuri said a surface-to-surface missile or an air-to-surface
missile could be equipped with PGMs.

A series of trials using a Remotely Piloted Vehicle
(RPV)
to simulate the speed of the mother missile while ejecting
the PGMs will be conducted at Balasore, Orissa, from March this year. Initially,
the RPV will be tested using two seekers—IIR (Imaging Infra-Red) and mmW
(millimetric wave) to track the target. Subsequently, the tests would be conducted
with RPV for separation of munitions. The technology demonstration of the
launch of a single PGM with multiple seekers from the RPV will be completed in
a year.

Dr. Chaudhuri said that one of the main reasons
for using an RPV was to reduce costs as it could be re-used.


He added that the
Research Centre Imarat (RCI) was also likely to collaborate withanother country for developing sensor-fused
munitions
. In this type, they sense the target and
fuse the warhead when the mother missile is in close proximity to the target.
He said work had already begun in that direction.


The Hindu : Today's Paper / NATIONAL : Multiple-target missiles to redefine warfare
 
IF we integrate Brahmos 1 and Brahmos 2 with this technology. These Missiles will become lethal and unstoppable hitting multiple targets. :cheers:

You mean something like CVS401-Perseus.
 
You mean something like CVS401-Perseus.

Yes mate, That is the reason the tech is being developed. One Brahmos fired from Su 30MKI can kill Destroyer or a Frigate, even though the ship may have surface to air defense systems.
 
very critical and sensitive technology. specially the integration and designing of electronics controlling the process. Will be a Master piece. And may be integrated into MIRVs too.
 
very critical and sensitive technology. specially the integration and designing of electronics controlling the process. Will be a Master piece. And may be integrated into MIRVs too.

It is MIRV only... Ain't it?
 
It is MIRV only... Ain't it?

This cannot be called MIRV. MIRV = Multiple Independently targeted Re-entry Vehicle.

For A2G missiles or cruise missiles, there is no re-entry because they never leave the atmosphere.

I think he means we should put this technology onto MIRVed warheads, where a supposed ICBM would
launch 6-10 MIRVs and each MIRV releases atleast 2 sub-warheads. Total 20 warheads on a 10-MIRV missile
can be fitted.
 
It is MIRV only... Ain't it?

Nope!

PGMs are miniaturised missiles with small seekers,
actuators and on-board computers and will be integrated with tactical missiles
having a range of 100-200 km.

Source: http://www.defence.pk/forums/indian...-missiles-redefine-warfare.html#ixzz2I3H6Qeye

MIRV means the job is to be finished by using the NUKES, whereas here no such case.
More, MIRV is much more complicated a technology than above.


MIRV: India


India has indigenously developed Redundant Strap down Inertial Guidance System (RESINS) which employ Dynamically Tuned Gyros (DTG) and Servo Accelerometer (SA) for its space program. The entire attachment should be small and light enough to constitute in missile due to its weight and size constrain, created challenges for engineers.
 

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