Indian Missiles and Munitions Discussion

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Kersi D
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Re: Indian Missiles and Munitions Discussion

Post by Kersi D »

Kakarat wrote:
Kersi D wrote: I just hope the pvt sector is allowed into serious defence production Last off topic post.
NAMICA was first developed by L&T.



The current NAMICA is from BEL

BEL & L&T were competitors, but L&T failed
What is BEL doing in developing ICVs ?

It may be BHEL.

K
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Re: Indian Missiles and Munitions Discussion

Post by rohitvats »

Bheem wrote:Manportable Spike/gill series, Kornet and Javelin are around US$ 100,000 per unit. Nag is much bigger missile more in the range of Spike ER or Hellfire. Rs. 335 crores with 13 launchers seem reasonable as around Rs. 50-100 crores would be for launchers alone. Then there should be reloading vehicles, ground support equipment, testing equipment etc. I would peg the cost of stand alone unit of nag missile at around Rs. 40-50 lakhs each, while comparitive western systeme should be around Rs. 50-75 lakhs each
In the comments sections of the Ajai's article on NAG+NAMICA, he mentioned that the cost (335 crores) also includes the cost of setting up the production line for the missiles. Another thing; though I'm not aware of optronics that go with NAMICA, considering the sophisticated nature of these sub-systems, would'nt their price itself be high? thanx.
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Re: Indian Missiles and Munitions Discussion

Post by krishnan »

Why are you people so much bothered about the cost? At least the money is going back into indian hands ( hope so)
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Re: Indian Missiles and Munitions Discussion

Post by manjgu »

krishnan.. good point. and guys pl dont compare cost of apples vs bananas. each system is different. i would buy only nags if each one of them promises to send 1 al khalid ( inshaallah) to its maker ! and 72 virgins

aise lag raha hai ki BR members ki jaib me se paise ja rahe hain !!
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Re: Indian Missiles and Munitions Discussion

Post by manjgu »

about this optical seeker... just curious how does it work if the tanks are putting up smoke?? any experts here
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Re: Indian Missiles and Munitions Discussion

Post by Kakarat »

Kersi D wrote: What is BEL doing in developing ICVs ?

It may be BHEL.

K
It is not BHEL but BEL which is developing NAMICA
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Re: Indian Missiles and Munitions Discussion

Post by a_kumar »

There was a discussion in previous pages on missiles for launchers..

X-posting from Defense R&D thread..
SriniY wrote:One more thing from the article

QUOTE
Q. What are the focus areas in the 25-year technology development plan?
A. There are three. The closest to our heart is low-intensity conflict (LIC). Many technologies that we have developed for the military have relevance for LICs. You will appreciate that many agencies in the country are today involved in LICs — the paramilitary forces, police forces, counter-insurgency and counter-terror organisations and so on. We have started a programme to customise DRDO technology for each of them. LIC is one of our key result areas now.
Another area is space security because future wars are going to be controlled from space as network-centric warfare becomes the new way of war-fighting. So, technologies that are relevant for space security such as ballistic missile defence, anti-satellite systems, are going to be part of our development process. Secondly, to be able to quickly launch satellites to regain space-based capabilities when existing assets are attacked or denied to our military during war. These are low-cost, quick reaction satellite launch systems and low-endurance satellites — they last just long enough to do their job. What will emerge through our programme are micro-satellites, mini-satellites etc. On the launch side, some of our missiles can be modified, a satellite put on top of them and launched
/QUOTE
This probably has not been reported before
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Re: Indian Missiles and Munitions Discussion

Post by John »

Bheem wrote:Manportable Spike/gill series, Kornet and Javelin are around US$ 100,000 per unit. Nag is much bigger missile more in the range of Spike ER or Hellfire. Rs. 335 crores with 13 launchers seem reasonable as around Rs. 50-100 crores would be for launchers alone. Then there should be reloading vehicles, ground support equipment, testing equipment etc. I would peg the cost of stand alone unit of nag missile at around Rs. 40-50 lakhs each, while comparitive western systeme should be around Rs. 50-75 lakhs each
Actually the western systems like PARS 3 cost far more than that (1/2 million to be exact)

krishnan wrote:Why are you people so much bothered about the cost? At least the money is going back into indian hands ( hope so)
Well cost is very important if IA plans to mass procure Helina, if it turns out to be cheaper it will likely replace Vikhr and other missile which are not at NEOL.
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Re: Indian Missiles and Munitions Discussion

Post by ramana »

a_kumar wrote:There was a discussion in previous pages on missiles for launchers..

X-posting from Defense R&D thread..
SriniY wrote:One more thing from the article

QUOTE
Q. What are the focus areas in the 25-year technology development plan?
A. There are three. The closest to our heart is low-intensity conflict (LIC). Many technologies that we have developed for the military have relevance for LICs. You will appreciate that many agencies in the country are today involved in LICs — the paramilitary forces, police forces, counter-insurgency and counter-terror organisations and so on. We have started a programme to customise DRDO technology for each of them. LIC is one of our key result areas now.
Another area is space security because future wars are going to be controlled from space as network-centric warfare becomes the new way of war-fighting. So, technologies that are relevant for space security such as ballistic missile defence, anti-satellite systems, are going to be part of our development process. Secondly, to be able to quickly launch satellites to regain space-based capabilities when existing assets are attacked or denied to our military during war. These are low-cost, quick reaction satellite launch systems and low-endurance satellites — they last just long enough to do their job. What will emerge through our programme are micro-satellites, mini-satellites etc. On the launch side, some of our missiles can be modified, a satellite put on top of them and launched
/QUOTE
This probably has not been reported before

I would like to know the weight of this quick launch satellites. Kalam saab used to talk about launch a sat from Agni series.
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Re: Indian Missiles and Munitions Discussion

Post by ramana »

Brig G. Kanwal acknowledges Arun on page two:
http://forums.bharat-rakshak.com/viewto ... 24#p835624

Thanks sirji!
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Re: Indian Missiles and Munitions Discussion

Post by ankit-s »

I would like to know the weight of this quick launch satellites. Kalam saab used to talk about launch a sat from Agni series.


Agni III has 2.5 tons of cargo capacity (payload), our heaviest INSAT so far ejected into the orbit is 2.2 tons, the job seems to be doable.
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Re: Indian Missiles and Munitions Discussion

Post by shukla »

Abandoned ammunition explodes, kills three children in HP
SHIMLA: Three children were killed when abandoned ammunition exploded near an army firing range in Himachal Pradesh's Kangra district, police said on Wednesday. The children were trying to remove scrap from the used mortar shells. "Three children, aged 10 to 12 years, were killed on Tuesday when they tried to break the used shells of mortars near the army firing range," Deputy Superintendent of Police Jeet Singh told IANS on phone.

He said the children collected the shells from the firing range and tried to break it to recover scrap and lead. One of the shells exploded and killed them on the spot. "We have recovered three more shells from the spot," he said
That so sad.. Wonder if the ammo wasn't disposed off properly?
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Re: Indian Missiles and Munitions Discussion

Post by ankit-s »

Kersi D wrote:
Kakarat wrote:
What is BEL doing in developing ICVs ?

It may be BHEL.

K
It is BEL.

http://livefist.blogspot.com/2008/08/ph ... -atgm.html
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Re: Indian Missiles and Munitions Discussion

Post by AdityaM »

newbie questions:
Why should one use a missile to launch a sat and not a proper launcher?
Is it cheaper? is it because many missiles are always available while rocket needs to be created specifically for a mission?
Better to use a missile than let it age?
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Re: Indian Missiles and Munitions Discussion

Post by Marut »

ankit-s wrote:I would like to know the weight of this quick launch satellites. Kalam saab used to talk about launch a sat from Agni series.


Agni III has 2.5 tons of cargo capacity (payload), our heaviest INSAT so far ejected into the orbit is 2.2 tons, the job seems to be doable.
Not so fast. Based on my rudimentary understanding or orbital mechanics and satellite launch, all satellites need to placed in orbit with an injection velocity to enable their progression on the orbit. So you can't load the missile upto its gills. Another factor is the size of the satellite, since it needs to fit within the RV design of the missile.

From prior discussions about this, I recall that the satellites will probably be in the nano, micro & mini sats category with polar orbits. Think something similar to TES and its ilk :wink: Geostationary sats will need the GSLV just as bigger polar sats will need the PSLV.
AdityaM wrote:newbie questions:
Why should one use a missile to launch a sat and not a proper launcher?
Is it cheaper? is it because many missiles are always available while rocket needs to be created specifically for a mission?
Better to use a missile than let it age?
Newbie answers :)

Your hunches are correct.

It should be cheaper to launch the smaller sats using missiles since missiles are multiple compared to launch vehicles which are minuscule in numbers. Another factor is the time required. Prepping for a space launch is time consuming with a longer lead time than fitting a sat on the missile for launch. Also if you have a few lighter sats, you need not wait for more to make it cost effective for the payload capacity of the launch vehicle. The missile maybe a better alternative. Again if the lighter sat is a critical one with urgent need, missile launch will be quicker and cost effective. JM2P
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Re: Indian Missiles and Munitions Discussion

Post by csharma »

How reliable are the ranges for Agni III and IV (V) that are quoted by Gurmeet Kanwal. I notice he is using 1.5 tonne payload.
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Re: Indian Missiles and Munitions Discussion

Post by ankit-s »

Not so fast. Based on my rudimentary understanding or orbital mechanics and satellite launch, all satellites need to placed in orbit with an injection velocity to enable their progression on the orbit. So you can't load the missile upto its gills. Another factor is the size of the satellite, since it needs to fit within the RV design of the missile.


Fast I was with one liner without going into a nitty gritty. But it is a common sense that although many of the technological building blocks involved in (space launch vehicles) are the same as those required to develop long-range ballistic missiles yet there got to be fine tuning of other mechanisms involved into ejection process of the satellite, considering the fact that missiles are not meant for satellite placing in orbit.

A dedicated space launch vehicle uses payload fairing, different from missiles which contain warheads (meant for explosion) under the cone. Without payload fairing (which is discarded) how would you eject a satellite into the orbit anyway since the missile dont have them.

The 49 m tall GSLV has abt 8 meter payload fairing, while the total length of Agni III is 17 meters. Hence there got to be modifications.
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Re: Indian Missiles and Munitions Discussion

Post by neerajb »

In new missiles, the Astra air-to-air beyond visual range missile has undergone four to five ground launch trials. We are now qualifying its infra-red seeker. Once ready, it will go on multiple platforms, including Tejas and Sukhoi fighters.
http://www.bharat-rakshak.com/NEWS/news ... wsid=12501

This is news to me.

Cheers....
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Re: Indian Missiles and Munitions Discussion

Post by KrishG »

ankit-s wrote:I would like to know the weight of this quick launch satellites. Kalam saab used to talk about launch a sat from Agni series.


Agni III has 2.5 tons of cargo capacity (payload), our heaviest INSAT so far ejected into the orbit is 2.2 tons, the job seems to be doable.
No Agni missile as of know can launch satellites. A modified Agni-III with a 3rd stage should be able to launch small satellites of around ~200-250 kg into LEO.
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Re: Indian Missiles and Munitions Discussion

Post by ankit-s »

KrishG wrote:
ankit-s wrote:I would like to know the weight of this quick launch satellites. Kalam saab used to talk about launch a sat from Agni series.


Agni III has 2.5 tons of cargo capacity (payload), our heaviest INSAT so far ejected into the orbit is 2.2 tons, the job seems to be doable.
No Agni missile as of know can launch satellites. A modified Agni-III with a 3rd stage should be able to launch small satellites of around ~200-250 kg into LEO.

No missile can launch a satellite unless modified. (check my previous post) You are limiting a payload to 250 Kg while I think the numbers may go even higher. At 200-250 Kg its not worth wasting Agni III, does not make economic sense because per Kg launch prices have come down anyway.
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Re: Indian Missiles and Munitions Discussion

Post by Rahul M »

have you people even read the report in which VKS is talking of launching sats by missiles ?
I doubt it. he is talking of launching small sats as a stop-gap measure if any of our sat gets taken out. economics, efficiency and all those buzzwords are irrelevant in those cases.
Secondly, to be able to quickly launch satellites to regain space-based capabilities when existing assets are attacked or denied to our military during war. These are low-cost, quick reaction satellite launch systems and low-endurance satellites — they last just long enough to do their job. What will emerge through our programme are micro-satellites, mini-satellites etc. On the launch side, some of our missiles can be modified, a satellite put on top of them and launched
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Re: Indian Missiles and Munitions Discussion

Post by KrishG »

ankit-s wrote: No missile can launch a satellite unless modified. (check my previous post) You are limiting a payload to 250 Kg while I think the numbers may go even higher.
Do you expect is to be able to launch all of it's 2.5 tons of payload into LEO ?? :roll:
ankit-s wrote:At 200-250 Kg its not worth wasting Agni III, does not make economic sense because per Kg launch prices have come down anyway.
Agni III wasn't built to launch satellites.
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Re: Indian Missiles and Munitions Discussion

Post by D Roy »

most of the "modifications" required to turn BMs into responsive space launch vehicles are on the software side of things.

Of course an additional booster engine is also incorporated sometimes for certain orbits.
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Re: Indian Missiles and Munitions Discussion

Post by jaladipc »

Inorder to launch a satellite using A-III into LEO,it is highly possible with slightly few modifications

Before that,one has to know the true specifications and capabilities of A-III

A-III as of today can throw a wieght of ~2500 Kg to a distance of > 3500km by touching a peak altitude of 350km.

Having said that,it 2m dia maynot be plausible always to put a desired sat in orbit (~500km).Hence its RV needs to be modified to accomodate a payload faring of 3m dia atleast in the most hypothetical scenario.
The trade off between payload and altitude needs to be utilised to achieve significant altitude.It may also need a HAM( or small booster) to put the sat into the desired LEO.

A RV weighs more than a payload faring.Hence some mass improvements can be achieved.

Afterall,it is highly possible to put a ~1000kg or less into a 500km LEO.
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Re: Indian Missiles and Munitions Discussion

Post by symontk »

Moreover the Agni-3's first stage solid booster has 3 segments, it can be uprated to 5 segments easily creating a 75 ton first stage (current one has total weight around 40-45 tons, each segment having around 15tons). This would greatly enhance the payload capacity.

As a topping you can add the prthvi first stage and then a liquid engine for satellite deployment

Maybe the Agni-4 is such a combination and thats why its not referred as a missile. :wink: :idea:
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Re: Indian Missiles and Munitions Discussion

Post by ankit-s »

Do you expect is to be able to launch all of it's 2.5 tons of payload into LEO ??

I still abide by my previous wordings: I think the numbers may go even higher. (more than 250Kg)



Agni III wasn't built to launch satellites.

Read my post of 8:48 AM before you posted this: Missiles are not made to place satellites into orbit.
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Re: Indian Missiles and Munitions Discussion

Post by a_kumar »

ankit-s wrote:At 200-250 Kg its not worth wasting Agni III, does not make economic sense because per Kg launch prices have come down anyway.
How did you arrive at above? It would be interesting to know whats the cross-over point for payload, where using missiles cease to be economical.
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Re: Indian Missiles and Munitions Discussion

Post by ankit-s »

D Roy wrote:most of the "modifications" required to turn BMs into responsive space launch vehicles are on the software side of things.
A 3 stage vehicle whose Re-entry Vehicle is to be modified means one third of change coming only to hardware part itself. Then - in order for missile to reach LEO, you have to probabily modify its first stage for adequate thrust. I see more hardware here viz; replace the nose cone of such missile with payload fairing, which splits (vertically) open by way of pyro separation bolts at abt 120 KM, and for that you have to employ automatic timers to ignite the bolts.


Please see how crucial is PF when it comes to satellites launching:
Payload fairing is one of the main components of a launch vehicle.

In 1999, the launch of the IKONOS-1 Earth observation satellite failed after the payload fairing of the Athena rocket did not open properly.

On February 24, 2009, NASA's Orbiting Carbon Observatory satellite failed to reach orbit after liftoff presumably because the fairing on the Taurus XL launch vehicle failed to separate, causing the vehicle to retain too much mass and subsequently fall back to Earth; it landed in the Indian Ocean near Antarctica.

The same happened to the Naro-1, South Korea's first carrier rocket, launched on 25 August 2009. During the launch half of the payload's fairing failed to separate, and as a result the rocket was thrown off course. The satellite did not reach a stable orbit
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Re: Indian Missiles and Munitions Discussion

Post by ankit-s »

a_kumar wrote:
ankit-s wrote:At 200-250 Kg its not worth wasting Agni III, does not make economic sense because per Kg launch prices have come down anyway.
How did you arrive at above? It would be interesting to know whats the cross-over point for payload, where using missiles cease to be economical.


PSLV costs 17 million USD flyaway cost for each launch.

http://en.wikipedia.org/wiki/Polar_Sate ... ch_Vehicle

What would be the relative cost of modified Agni III equipped with such a job of placing a satellite into a LEO orbit?

We have the following on per Kg price:
ISRO won the contract to launch the Italian satellite, amidst stiff competition from other countries. As per estimates made by Antrix Corp, the commercial arm of the ISRO, the cost in the international market of launching commercial satellites into the polar orbit is about Rs13, 000-15,000 per kg and about Rs20, 000 per kg in the geo-stationary orbit.
http://www.financialexpress.com/printer/news/197384/

Now you do the math @ 250 Kg and see whether Agni III is expendable!
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Re: Indian Missiles and Munitions Discussion

Post by kit »

I guess that would be ok if there is an emergency strategic imperative in a war scenario where indian satellites are knocked out.
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Re: Indian Missiles and Munitions Discussion

Post by svinayak »

kit wrote:I guess that would be ok if there is an emergency strategic imperative in a war scenario where indian satellites are knocked out.
What about capability to lauch multiple satellites within a short time. Such as 10 satellites within 30 days.
What about the protection of the launch sites so that in the event of war enemy could knock of the lunch sites. Does India have redundancy in the launching capacity
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Re: Indian Missiles and Munitions Discussion

Post by abhik »

According to AJ's article it seams as though the helo launched nag only has 'terminal guidance' i.e. its seeker does not work at full range(7000m?, but only to about 4000m which is the range of the Namica launched version),so to make up for this limitation it has to be guided manually via some sort of datalink until the missile can acquire the target.This obviously means that firing a salvo of missiles at a group of targets will take a lot longer than for true 'fire and forget' missiles like the hellfire(with MMW seeker) and PARS 3lr. So the question is will it not be a better compromise to have cheaper laser guidance system(possibly from the indigenous LAHAT type of missile which they have been showing def-expos for quite some time ) without the datalink until a full range seeker is developed.
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Re: Indian Missiles and Munitions Discussion

Post by ramana »

Quick launch of sats is a wartime requirement. So if Agni series can do that is well and good.No one is talking of commerical launches so take it easy.

Anyway asking experts, the AIII capability to launch to 400km orbit ie ~200nm is 700kg. Assumption is that there is a small upper stage (like ASLV 4th stage) for orbital injection.
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Re: Indian Missiles and Munitions Discussion

Post by Kanson »

I dont have hard data, but Agni-3 costs around 50 Crores. It depends upon the costing method as well.

Ramana: fwiw, sats that Saraswat is taking abt are in 100kg range for Agni-3. Look for IMS-1 type sats for this role. Or clusters with decentralised missile modules could be used. It will be for tmp purpose in the time of war so it will be designed accordingly; not like other Sats with years of operational life, JMT.
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Re: Indian Missiles and Munitions Discussion

Post by jaladipc »

A-III costs ~42 crore while PSLV(latest version) costs ~120 crore Rs as per Dec-2009

The satellite launching market world wide is of billions of dollar.And space agencies/companies dont launch heavy sats all the time.Hence a major share does go to small ,medium,micro,nano sats.

IF we employ BM route to launch sats,the primary advantages are:-

Can go for mass production
Obviously brings down the production cost for both the agencies and customers
As a spin off reduces the burden on strategic forces due to mass production and keeps mass attack option open(with minor modifications)
Provides a launch window at any time of the year(dont necessarily have to wait for VAB to become free for next rocket assembly and stuff)
Improves the QA for strategic missiles due to mass procurement
.
.
.
.
If GOI/ISRO/DRDO wants to achieve something significant, they will have another option in the name of sea launch.

And the platform will be virtually ready in the name of Viraat.
Once viraat is decomissioned,and gets a minor refit to accomodate the control systems and sea launch type rail launcher- A-III/A-IV/A-V can be easily accomodated while even having another as spare in the lower deck.Propell the ship to the equator for ideal equatorial launches.IMHO a very most cost effective launching system for a budget oriented nation like India if all the possible options are exercised.

At the end of the day only The WILL to DO is needed.
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Re: Indian Missiles and Munitions Discussion

Post by Rahul M »

Acharya wrote:
kit wrote:I guess that would be ok if there is an emergency strategic imperative in a war scenario where indian satellites are knocked out.
What about capability to lauch multiple satellites within a short time. Such as 10 satellites within 30 days.
What about the protection of the launch sites so that in the event of war enemy could knock of the lunch sites. Does India have redundancy in the launching capacity
that's a very good point. IMHO, launching from missiles would give you that redundancy provided alternate centres able to handle mating sats to missiles exist, which should be the case once we have the capability first.
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Re: Indian Missiles and Munitions Discussion

Post by ankit-s »

kit wrote:I guess that would be ok if there is an emergency strategic imperative in a war scenario where indian satellites are knocked out.

China is our worthy adversary vis a vis such a misadventure (Pakistan is no contest), and knowing that they can be paid back in the same coin, they would not come onto our space assets at the least as they know we can knock down their orbital assets.
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Re: Indian Missiles and Munitions Discussion

Post by Anurag »

First artist impressions of the Agni-V from LiveFist. Note the third stage is QUITE clear!

http://livefist.blogspot.com/2010/03/ex ... gni-v.html
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Re: Indian Missiles and Munitions Discussion

Post by ankit-s »

jaladipc wrote:A-III costs ~42 crore while PSLV(latest version) costs ~120 crore Rs as per Dec-2009

The satellite launching market world wide is of billions of dollar.And space agencies/companies dont launch heavy sats all the time.Hence a major share does go to small ,medium,micro,nano sats.
Something from the web world:
Euroconsult forecasts that the increased average weight of a commercial geostationary satellite will occur especially at the upper end of the scale. Among the current crop of commercial telecommunications satellites under construction are several consumer broadband and mobile voice and data spacecraft weighing well over 13,277 pounds (6,000 kg).

Euroconsult found that 3 percent of commercial satellites currently on order and scheduled for launch by 2011 will weigh more than 14,330 pounds (6,500 kg) at launch. Between 2012 and 2018, the report says, 13 percent of all commercial telecommunications satellites will weigh more than 14,330 pounds, while another 27 percent will weigh between 12,125 pounds and 14,330 pounds (5,500-6,500 kg).

These figures exclude Russian-built satellites that are designed to be launched only by Russian Proton rockets directly into geostationary orbit. Most non-Russian telecommunications satellites are heavier than their Russian counterparts and are placed into a transfer orbit by their launch vehicle. They then use their own fuel to climb into final geostationary position.

If Euroconsult is correct, 40 percent of geostationary satellites ordered between 2012 and 2018 will weigh more than 12,125 pounds, compared to 29 percent in the past three years and just 17 percent earlier this decade.

Satellites in the lowest weight class for geostationary orbit - 1,500 kilograms to 3,500 kilograms - will retain their current market share of 24 percent, according to Euroconsult. The midrange class of spacecraft, between 7,716 pounds (3,500 kg) and 12,125 pounds, will lose market share. Such satellites represent 47 percent of commercial geostationary satellites currently under construction. They are expected to account for 36 percent of the spacecraft built between 2012 and 2018.
International Launch Services is the U.S. based company with exclusive rights for worldwide commercial sales and mission management of satellite launches on Russia's premier vehicle, the Proton. ILS is a long-standing, successful U.S.-Russian venture with exclusive rights to the worldwide sale of commercial Proton launch services. Since its creation in 1995, ILS has signed contracts for more than 100 launches valued at more than US $8 billion. Following its first launch in 1965, Proton has launched more than 350 times. Current backlog is 23 Proton missions.
One of the most expensive things about a space launch is the fuel. For every pound of payload launched into low Earth orbit, 25-50 pounds of fuel is required. Typical rockets are fueled by a combination of liquid hydrogen and oxygen, which both must be kept at very low temperatures using many tons of cryogenic cooling equipment. Think of a rocket as a very expensive refrigerator the size of a tall building.
The most promising routes to substantially reducing launch cost involve solutions where the payload does not need to bring fuel along with it during the ascent. This is one of the most expensive elements of a conventional rocket launch — a rocket needs to carry enough fuel not just to propel the payload, but also the remaining fuel on the way up. The bottom of the atmosphere is the densest and most costly in terms of energy to navigate through, but this is also where the rocket itself is heaviest, necessitating very large fuel tanks.
Satellites have an operating lifespan between five and twenty years. Currently, the former Soviet states launch about 1,300 satellites into orbit per year, the USA about 1,000, Japan 100, China 50, France 40, India 30, the UK 25, and a few from Australia and Israel. The company Sea Launch — a consortium of four companies from the United States, Russia, Ukraine and Norway — launches a few satellites into orbit from international waters every year.
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Re: Indian Missiles and Munitions Discussion

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