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Subject: Redundancy US missile programs?
dwightlooi    8/11/2004 2:07:12 AM
It seems to me that the US is in the habit of having two or three programs that strive for similar goals and which can be merged into one system.

1) PAC-3 and SM-3. These two could have been one system. Or at least, the SM-3 could have used the PAC-3 airframe. It'll certainly fit into the Mk41 cell envelope. And it is arguably better than relying on the 40 year old TARTAR airframe.

2) THAAD can actually be a land and naval system the 37cm by 6 m THAAD airframe fits neatly into the Mk41 envelope too. And there is no reason why some variation of the missile cannot be put to sea.

3) The ESSM should have been a navalized AMRAAM from the beginning.

I am not saying that there aren't technical issues with adapting one system to another use, but whatever it is it'll be more economical than have two separate developments with similar objectives.
 
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Siddar    RE:Redundancy US missile programs?   8/11/2004 3:11:07 AM
The downside of haveing only one system is that you can end up granting a monopoly to one company and end up paying more money for lesser products in the end. Multipule companys that can both do the work sends clear message to companys that if they screw up are just dont put enough effort into project that they can be replaced.
 
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doggtag    RE:Redundancy US missile programs?   8/11/2004 7:42:06 AM
ESSM was never and is never going to be a navalized AMRAAM: The ESSM RIM-162 (Evolved, or Enhanced, SeaSparrow Missile) is a development/follow-on of the RIM-7 SeaSparrow family which has been in service since before AMRAAM was even conceived. And the 8inch diameter body of RIM/AIM-7 affords greater growth potential and usable volume (range + warhead) over the 7inch diameter of the AIM-120 series. Besides, ships aren't as limited by orcnance weight as aircraft (a key point in going to a smaller, lighter system when AMRAAM was considered to supercede Sparrow, which never really lived up to expectations anyway. That's the reason the UK developed the Skyflash "copy", and Italy developed the Aspide. They both look identical to Sparrow, but the innards are considerably better.) I believe that Norway was developing a navalized AMRAAM for lightweight air defense, but I'll have to look for it. And also, the ESSM current body planform vaguely resembles the "40 year old" Tartar airframe, just as the current Standard SM-2 series (the ill-informed may think ESSM is a scaled-down SM-2) The airframe isn't obsolete, but is an evolutionary design of several decades of US missile research. And ESSM uses thrust-vector control to augment its maneuverability. link link And considering how much Patriot PAC-2/3 tech went into the Standard SM-3 (or maybe the other way around...), it is interesting to note that both systems are still being procured. Of course, Raytheon owns the US missile monopoly, so anything to keep their bank rolls in the black keeps them happy... even if most of these systems overlap each other considerably (which technically, a truly effective ADA network, land or sea, should be capable of.).
 
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dwightlooi    RE:Redundancy US missile programs?   8/11/2004 3:28:51 PM
A couple of points.... 1) The SM-2 is getting rather long in the tooth. The airframe aside, it lacks a few key features that define the current generation of medium weight ship-to-air missile -- an active terminal seeker, track-via-missile 2-way data link and aerodynamically independent lateral jet attitude control (ala Aster, PAC-3). The AEGIS system has always been one with a great radar (for its time anyway and a so-so missile). 2) The AMRAAM is not just a reduced form factor sparrow. Other than aerodynamic differences, it is an active missile. ESSM can benefit from an active seeker which will relieve the missile directors of a lot of work and allow a much higher salvo rate against sea skimmers. 3) The SM-3 is a 3 stage rocket that basically uses the SM-2 AEGIS ER booster and missile to deploy a terminal kill vehicle payload. The THAAD missile is designed from the ground up as a 2-stage kinetic energy exo-atmospheric interceptor and it fits into a Mk41 cell with room to spare. Not considering a navalized version of the missile seems at the very least wasteful.
 
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doggtag    RE:Redundancy US missile programs?   8/11/2004 4:09:15 PM
I don't intend to imply that I think AMRRAM is a "reduced form factor Sparrow". AMRAAM airframe/weight envelope was suggested/preferred over a product-improved Sparrow because of the necessity of weight constraints and larger numbers to be carried by (US) aircraft. The F-16 can and does carry AIM-120s on its wingtip rails, something it can't do with the 500+ lb Sparrow series. Plus, it can deploy a twin-rail underwing system for AIM-120, where it can only carry a Sparrow singly (typically, and F-16 could carry 4 Sparrow and 2 Sidewinder, or 8-10 AMRAAMs). And fortunately, all US and NATO aircraft who carry AIM-7 semi-conformally can also fit the AIM-120 (F/A-18, F-15, F-14, Tornado). There is still plenty of "room to grow" in both the ESSM and Standard SM/ER series missiles. The surface-to-air systems just have not been as upgrade-favored because we have foolish-thinking politicians and brass who may be implying our naval air assets will be effective enough, so our heavyweight naval SAMs have not gotten the top-of-the-line upgrade packages that could keep them at the top of the capabilities list (although the latest-produced SM-2s are far more superior than the first generations). I do agree that we do need a navalized missile that is on par with the suggested performances of the S-400 system, if not better (more capable against all-altitude targets, including ballistic and sea-skimming capabilities...and it shouldn't need to be the seriously expensive SM-3 variant, which would not be used against very-low-level threats...hence the need for ESSM). The 13.5inch diameter main body of Standard is certainly sufficient to pack in the necessary technology. link There are sufficient sites available with unbiased capabilities statements to both the ESSM and latest Standard missile systems. Agrreably, both would be far superior with further upgrades. But a naval AMRAAM does not offer the growth potential of the ESSM body, even if it has such a promising-performing seeker/guidance section (no reason it couldn't be retorfitted into the ESSM at some future date). Besides, ESSM's primary requirement was very low level/anti-sea skimmer operation (which again, the SM-3 won't be used for); AMRAAM was designed for more low-to-medium altitude work and shoot-down modes (not becoming its own sea-skimming anti-missile missile like ESSM can do)..
 
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Roman    RE:Redundancy US missile programs?   8/11/2004 4:44:26 PM
You never know what countermeasures the enemy will come up with, so it makes sense not to depend on a single system, as any one system may prove very vulnerable to a particular unforseen countermeasure.
 
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dwightlooi    RE:Redundancy US missile programs?   8/11/2004 9:16:42 PM
Funny thing... They are actually planning a Standard with the AMRAAM seeker and the AIM-9X/ASRAAM IR seeker. Tentatively called the SM-6 though that is weird given that SM-4 and SM-5 are yet unassigned. In essence it'll do what the SM-2MR Block IIIB does at greater ranges, over land or under the radar horizon. The active radar and IR seekers allow for speculative launches at targets that cannot be illuminated by the SPG-62 directors -- such as approaching sea skimmers that are under the horizon. The long ranged ones normally fly a hi-lo trajectory where they fly at high altitude for range performance but pop down to wave height for the last 100km or so to avoid interception. Normally airbourne or ship bourne sensors can pick them up after launch, but they pop down off the screens before weapons and be employed against them. So rather than waiting for them to break radar horizon at 40km, salvos of "SM-6" missiles can be hurled in their direction. The missiles will not only seek and destroy the incoming missiles if they find them, but also provide radar info on what is over the horizon by relaying basic info from their active seekers back to the ship via a low-bandwidth, SW, 2-way radio link.
 
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Adamantine    RE:Redundancy US missile programs?   1/9/2005 3:09:51 PM
There is no real redundancy. SM-3 has three stage and the kill vehicle has significantly higher speed than THAAD. PAC-3 is not even in the same category for atbm purpose. In fact a larger diamter block 1 and bloack 2 SM-3 will be build to increase the speed further In order to intercept longer range , higher reentry speed ballistic missile at largert standoff range and higher attitude, you need BIGGER missile with better kinematic. SM-3 block 1A is 3309 pound. A Thaad is only 1200 pound. The kill vehicle kinematic performance is determind by speed and its lateral maneuvrability. A high speed heavy kill vehicle has more fuel to maneuvre and more electronic to discriminate target. SM-3 block 3 may use a 27 inch motor and will be a far heavier missile that cannot even fit into the current mk41 launcher. Probaly the navy will only build the block2 missile which has a full body 533 mm diamter airframe. ESSM has almost nothing to do with sparrow in terms of airframe despite the name. The new missile has a motor that is one inch larger in diameter and ur weighs 600 plus to 700 pound. Its 9inch motor with a 8 inch seeker missile. This missile use better airframe, higher energy propellant and modern electronic. almost nothing in common with sparrow except maybe the seeker. This missile could easily use a AMRAAM active seeker or some new AESA radar or huge diameter IR seeker (scale up version of aim-9x). AMRAAM when launch from ship when have a range of 18km. Maybe agianst slow flying incoming plane, it could intercept the target at 40km. ESSM could destroy fat agile target at 50 plus km. There is no way a tiny AMRAAM could have that kind of kinematic performance. If cost is not a issue, ESSM could be fitted with AMRAAM seeker without much hassle PAC-3 can intercept both short range ballistic missile and also AIRCRAFT. Its function is different from SM-3 which is used only for high attitude interception of missile. The kill vehicle in THAAD and SM-3 cannot be used in low attitude and is not design to kill aircraft although it some special situation, you can try using it to hit a very high flying MIG-31. It may work but its not design for this task. What US need is an equivalent of the S-400 to kill aircraft at 400km range. SM-6 fits the bill. US Army should procure some SM-6 to enable it to destroy enemy aircraft at very long range. For landbase application, SM-6 could have a lengthened booster. The current mk-41 does not permit SM-6 to e longer than 6.55 meter. A 5 meter booster could extend SM-6 max range to 600-700km and NO ESCAPE ZONE to 150km against all known aircraft (excluding SR-71). MK-41 cell is very small compare to the tube that house SA-12B giant missile. Thats the tyranny of dimension and constraint. Using modern technology, US could easily creat a 700km missile that weigh no more than 2.5 ton. Still much lighter than SA-12b which is rated at between 3300kg to 4500kg
 
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stinger       2/23/2008 9:45:02 PM
What has a longer range the AIM-120 or the ESSM?
 
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gf0012-aust       2/23/2008 10:09:00 PM

What has a longer range the AIM-120 or the ESSM?


Just a suggestion.  People will get brassed off if you ask questions that basic research could provide. 
 
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benellim4       2/23/2008 11:29:22 PM
I just skimmed this thread from the dead. The basic idiocy contained herein brasses me off. (Not you stinger.)
 
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Herald12345       2/24/2008 12:19:18 AM

I just skimmed this thread from the dead. The basic idiocy contained herein brasses me off. (Not you stinger.)

Yep-especially about ASTER, STANDARD, and ESSM.

Two missiles underestimated as to modernity and EFFECTIVENESS, and a PoJ even remotely compared in quality to them.

The ESSM has as much to compare NOW to the original dog, SPARROW, as the latest STANDARD II to the original TARTAR.

Evolution is not obsolescence.

Herald
 
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dwightlooi       2/26/2008 11:20:55 AM

What has a longer range the AIM-120 or the ESSM?


There is really no comparison between the two, the ESSM has almost 2.5 times the kinematic performance of the AIM-120. When fired from a zero-zero condition, an AMRAAM is 20~25km SAM. The ESSM goes to over 50km. When fired from a zero-zero condition, the AMRAAM typically goes about Mach 2.5. The ESSM reaches in excess of Mach 4. The ESSM is essentially the forward one-third of the sea sparrow grafted to a 10" rocket motor, controls shifted from the wings to the tails.

The advantages of the ESSM over missiles like the Aster 15 is that it is a single stage weapon (which allows for a shorter minimum range) and it is designed specifically for packaging density (a single Mk41 VLS cell holds 4 ESSMs). The weapons has demonstrated lethality against seaskimming AShM targets including maneuvering supersonic targets.

The ESSM is a semi-active homing missile. The decision to stay with SA homing is based on many reasons. The first being that in a horizon range weapon, there is no illuminator horizon issues. The second being it places target discrimination on the ship instead of leaving it up to the much more limited electronics you can pack in a missile. The third being that a powerful illuminator or multifunction radar on a ship is much more resistant to ECM than an tiny active seeker running on batteries. Finally, there is of course the direct compatibility with legacy sea sparrow control hardware already in service. The only disadvantage is the need for illuminator time from the launching vessel. The problem is really a non-issue on bigger, better equipped ships like the AEGIS destroyers with 3D radars. The ESSM is guided via inertial autopilot and datalink updates for most of its flight, and with three illuminators and each missile needing illumination only for the last 6 to 8 seconds of the engagement means that about 22 to 30 ESSM shots per minute -- which is more than is tactically likely. It is also a non-issue with X-band AESA equipped vessels like the German frigates using this weapon which can perform interrupted continuous wave illumination for the a practically unlimited number of ESSMs while time sharing or beam splitting for other radar tasks. However, in older, lesser ships with only one mechanical tracker/illuminator and a 2D air search radar the SA homing model limits the vessels to about 2 shots per minute because the lack of 3D positional updates means that the ESSM has to be fired in semi-active all the way mode with one dish per missile dedication until impact.
 
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doggtag    difference between a RIM- and an AIM-   2/26/2008 12:55:06 PM




What has a longer range the AIM-120 or the ESSM?




There is really no comparison between the two, the ESSM has almost 2.5 times the kinematic performance of the AIM-120. When fired from a zero-zero condition, an AMRAAM is 20~25km SAM. The ESSM goes to over 50km. When fired from a zero-zero condition, the AMRAAM typically goes about Mach 2.5. The ESSM reaches in excess of Mach 4. The ESSM is essentially the forward one-third of the sea sparrow grafted to a 10" rocket motor, controls shifted from the wings to the tails.

Good points.
But, take into effect that,
from its onset,
AMRAAM (AIM-120) was intended as an air-to-air weapon.
In that envelope, its range is in excess of any surface-launched ESSM (RIM-162).
 
Not then that there equates an even fair comparison: naturally, a smaller-diameter missile like the 7" AMRAAM (or even Aster) could even come close to compraing the range achievable in the 10" main-body-diameter ESSM.
(Perhaps somewhere should propose an air-launched ESSM, just to see actually how far range-wise it could compare to an AMRAAM...? Then we'd have a fair comparison.)
Mind you though: an air-launched ESSM might be the perfect start point for a non-air-breathing long range AAM that, effectively, fills the role left vacant by Phoenix (AIM-54) in the USN (not that they deem that role specifically needs filled by something more capable than an AMRAAM,..yet. But both the range and warhead potential are there).
 
Then again though: Sparrow was originally an air-to-air missile, even if considerably mediocre in performance,
but became a very formidable weapon when developed into the surface-launched Sea Sparrow.
(...or maybe it was just superior marketing by the US upon NATO, seeing as we don't have any Sea Flash (Sky Flash was UK's Sparrow replacement), even though Italy has successfully adopted their Aspide (their Sparrow replacement) into a surface-launched SAM weapon, and developed it further into the Sea Killer anti-ship/surface attack variants, with some featuring a 50+kg warhead in an enlarged forward section, IIRC)).
 
Naturally, anything with a diameter larger than 7" (and length longer than 12&1/2 feet) is going to have the potential to always be able to outrange (and carry a larger payload than) anything that does use a 7" diameter.
So don't expect any AMRAAM variants to ever surpass ESSM, as any electronics wonders and rocket motor tech packed into AMRAAM could just as readily be engineered to fit into the larger ESSM and allow it to keep a considerable margin in capability above its smaller brethren (both of 'em are Raytheon stablemates).
Same as how any given Standard (current in-service rounds) are always going to be capability-superior to ESSMs.
 
Depending on how well the Norwegians continue to develop, and market, their NASAMS system that uses surface-launched AMRAAMs, they may or may not be able to upset the Sea Sparrow's predominance (Aster is still an inch less in diameter than Sea Sparrow's 8").
 
In some smaller vessels, ESSM isn't going to be one-for-one exchangeable for Sea Sparrow: in VLS cells, it can be.
But for anyone still using those eight-round trainable launchers, the ESSM is too big (weight and volume).
But a newer-technology surface-launched AMRAAM (in NASAMS or even modified SLAMRAAM guise) may prove more of an asset worth purchasing than it would be to hang on to older-generation Sea Sparrows whose electronics haven't been upgraded comparably.
There's little reason that any surfaced-launched AMRAAM can't occupy the same cubic space aboard any Sea Sparrow launcher.
But is the reduced warhead of an AMRAAM (20-25kg?)  when compared to the Sea Sparrow's (30-40kg?) worth the gain in using updated electronics that may improve engagement abilities?
 

 
 
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benellim4       2/26/2008 5:44:59 PM
In some smaller vessels, ESSM isn't going to be one-for-one exchangeable for Sea Sparrow: in VLS cells, it can be.
But for anyone still using those eight-round trainable launchers, the ESSM is too big (weight and volume).
 
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Herald12345    Until somebody redesigns it like they are doing with the Block III SM-6   2/26/2008 5:50:25 PM
the ESSM killbody is still an 8"  diameter tube on a 10" booster.

Herald.
 
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