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Top ARM missile

Kh-31PD

http://sdelanounas.ru/i/a/s/aS5mbGFtYmVyLnJ1L2ZpbGVzL3N0Mi8xMjExOTIyNTU0LzEyNTE4NDA0Mzhfby5qcGc_X19pZD0yMTYwMQ==.jpg

Also Known As: AS-17 Krypton Mod 2

Origin: Russia

Contractor/s: Tactical Missiles Corporation (KTRV)

Description: The Kh-31, AS-17 Krypton NATO-codename, is an advanced, long range, highly supersonic missile designed to withstand countermeasures effects. The Kh-31 propulsion system consists of a solid-fuel rocket engine which accelerates the missile to Mach 1.8 airspeed. Then this engine is dropped and a jet engine ignites using the missile’s within space as a combustion chamber. The missile accelerates to Mach 3+ thanks to the jet engine.

The Kh-31PD is a long range, high speed, anti-radiation missile intended for engaging radar stations of air defense systems from distances of up to 250 kilometers with the carrier aircraft flying at 1.5 Mach and 15,000 meters of altitude. The guidance system combines inertial navigation system and broad band passive radar seeker. It is fitted with a 110 kg multiple charge, multi-purpose warhead. The Kh-31PD as a longer range version of the Kh-31P can be released primarily from Su-30MK, Su-34, Su-35, Mig-29K, Mig-29KUB and Mig-35 fighter aircraft. The Russian Tactical Missiles Corporation (KTRV) announced the existence of this weapon in 2009.

Parent system is the Kh-31
IOC: 1988
Other Family Members: Kh-31A, Kh-31AD, Kh-31P and Kh-31PK

http://s14.postimg.org/esrdl7mip/image.jpg

AGM-88E AARGM

<img src="http://baodatviet.vn/dataimages/201306/original/images1231231_Australia_mua_ten_lua_AGM_88E_doi_pho_datviet.vn_01.jpg" alt="http://baodatviet.vn/dataimages/201306/original/images1231231_Australia_mua_ten_lua_AGM_88E_doi_pho_datviet.vn_01.jpg" style=";" />

The AGM-88E AARGM is a medium-range air-to-ground missile developed by Alliant Techsystems (ATK). The primary role of the missile is to target enemy air defences. The missile can engage relocatable Integrated Air Defence (IAD) targets and other targets equipped with shutdown capability.

The AGM-88E AARGM is a follow-on to the US Navy’s AGM-88 High-Speed Anti-Radiation Missile (HARM). It will be the only tactical extended-range, supersonic, multi-role strike weapon in the US and Italian inventory when operational in 2012.

In September 2012, ATK received a $71m contract from the US Navy for the full-rate production of the AGM-88E AARGM.

The Advanced Anti-Radiation Guided Missile (AGM-88E) will be deployed by the US Navy, US Marine Corps and Italian Air Force.
AARGM development
“The missile can engage relocatable Integrated Air Defence (IAD) targets and other targets equipped with shutdown capability.”

The AARGM is being developed under a US and Italian joint acquisition programme led by the US Navy. The AARGM Advanced Technology Demonstration (ATD) Small Business Innovative Research (SBIR) Phase I commenced in 1990. The second and third phases began in 1991 and 1995 respectively.

In June 2003, ATK received a $223m contract to develop the AARGM. In November 2005, the Italian Ministry of Defence and the US Department of Defence signed a memorandum of agreement for the joint development of the AGM-88E AARGM. An MOU between ATK and MBDA was signed in July 2007 to evaluate possible work share opportunities with the German Ministry of Defence on the AARGM programme.

The missile was granted Milestone C approval for Low Rate Initial Production (LRIP) in September 2008. The Independent Operational Test and Evaluation (IOT&E) commenced in summer 2009.

The hardware and software deficiencies discovered in developmental testing and during its first IOT&E attempt in Q4 2010 were corrected during developmental testing. An integrated developmental/operational test (IT) period was concluded by July 2011. An operational test readiness review was conducted by The Operational Test Authority in July 2011.

By September 2011, the US Navy completed 40% of planned operational test flights, accumulating over 150 hours of missile operating time. It fired a total of four missiles at actual and simulated threat targets and emitters during the IT and IOT&E in 2011. The system maturity and reliability of the AARGM were checked in over 200 Beech King Air flight tests and 58 Captive Carriage FA-18 tests conducted against a wide range of targets.
AGM-88E design details
Related project
Ticonderoga Class Aegis Guided Missile Cruisers

27 Ticonderoga class (CG 47 – CG 73) Aegis guided missile cruisers were built between 1983 and 1994 by Ingalls Shipbuilding (now Northrop Grumman Ship Systems) at Pascagoula, Mississippi and Bath Iron Works (a General Dynamics Company), Bath, Maine.

The AARGM incorporates a new guidance section and modified control section combined with Rocket Motor and Warhead Section, wings and fins of HARM. The missile uses a multi-mode seeker to counter enemy shut-down capability.

The fire and forget capability of the missile allows weapon engagement at sufficient stand-off ranges. The Weapon Impact Assessment (WIA) subsystem supports battle damage assessment decisions by transferring impact assessment data prior to an impact.

The missile has a length of 417cm, diameter of 25.4cm and a wingspan of 112cm. The weight of the missile is 361kg. It can intercept targets within the range of 60+ nm while travelling at a speed of Mach 2+.

The AARGM can be integrated on the FA-18 C/D, FA-18 E/F, EA-18 G, and Tornado ECR aircraft. It is also compatible with the F-35, EA-6B, and F-16 aircraft.
Guidance and navigation
“The missile receives tactical intelligence information through an embedded Integrated Broadcast System Receiver (IBS-R).”

The AGM-88E is equipped with an advanced multi-sensor system comprising a Millimetre Wave (MMW) terminal seeker, advanced Anti-Radiation Homing (ARH) receiver and Global Positioning System/Inertial Navigation System (GPS/INS). The system can quickly engage traditional and advanced enemy air defence targets as well as non-radar time-sensitive strike targets.

The missile receives tactical intelligence information through an embedded Integrated Broadcast System Receiver (IBS-R). The IBS delivers situational awareness information and second source confirmation for the war-fighters. The missile transfers real-time weapon impact assessment reports. It offers extended-range engagement, as well as organic, in-cockpit emitter targeting capability, and situational awareness.
Propulsion

The AGM-88E AARGM is powered by an AGM-88 rocket motor using a Thiokol dual-thrust solid propellant.

http://s11.postimg.org/jx0scor6b/image.jpg

YingJi-91 (Kh-31P) Anti-Radiation Missile

http://img3.bbs.163.com/new/20091115/mil/hx/hxgcxy/3e524f599e37977ba826772d4288cbef.jpg

The Kh-31P (NATO reporting name: AS-17C Krypton-C) is the anti-radiation missile (ARM) developed by the Russian Zvezda Bureau, based on the Kh-31A (AS-17A) supersonic anti-ship missile. The PRC obtained some examples of the Kh-31P in the late 1990s, and is reportedly producing the missile locally as YingJi-91 (YJ-91). It is not known whether the YJ-91 production has been licensed by Russia. However, other sources suggested that the PRC imported some Kh-31P missiles from Russia between 2002 and 2004, possibly due to the delay in the YJ-91 development.

The PRC reportedly obtained several non-flying examples of the Kh-31P in the late 1990s for testing and study. This was confirmed by a photo published anonymously on Chinese Internet, showing a Kh-31P missile in a Chinese factory. It was reported that the PRC was developing YJ-91, a licensed copy of the Kh-31P, though the claim was denied by the Zvezda Bureau. During 2002~2004, the PLA reportedly purchased an unknown number of the Kh-31P missiles from Russia to arm its Su-30MKK fighters, which contradicts the previous report that an indigenous copy was being produced.

Click to enlarge
YJ-91/Kh-31P missile and Su-30MKK fighter in static display (Chinese Internet)

Nevertheless, either Kh-31P or its Chinese copy YJ-91 has been serving with the PLAAF since 2003~04. The missile provides the PLAAF with an advanced medium-range standoff anti-radiation strike capability, which was not previously possessed by the force. The Kh-31P was originally developed for the Soviet Air Force specifically against the U.S. Patriot air defence missile system. The missile is capable of suppressing enemy air defence systems and make its early warning ‘blind’ by striking their radar. Zvezda Bureau is also developing an improved 200km-range model which can directly attack enemy AEW or AWACS systems.

Design

The Kh-31P features a long slim cylinder body with a sharp nose, with four rocket boosters attached at the rear half of the missile. There are four clipped delta wings and four smaller tail surfaces of similar shape organised in cruciform configuration around the fuselage. Internally the L-112E radar seeker (D~F band) is in the nose with the guidance system, batteries and radio altimeter in the remainder of the front compartment, and the 87kg HE warhead immediately behind. A fuel tank, presumably with a kerosene-type fuel, occupies the area to the leading edges of the wing and the area almost to the rear edges is occupied by the ramjet. Much of the rear of the missile is occupied by a solid propellant booster through which runs the ramjet nozzle. Actuators are to be found below the tail surfaces.

Click to enlarge
An Internet source photo taken in 2000 showing a Kh-31P missile in a Chinese factory (Chinese Internet)

Propulsion

The Kh-31P features a unique dual propulsion system designed by the Soyuz Design Bureau in Turayevo near Moscow. First the missile is accelerated by its solid-fuel rocket engine to a speed of Mach 1.8, then the engine is discarded and the interior of the missile is converted into the combustion chamber of the missile’s jet engine. The latter accelerates the missile to a speed of almost Mach 4.5, while four air intake holes on the sides of the missile body open up.

Specifications

Length: 5.21m
Diameter: 0.36m
Wingspan: 1.15m
Weight: 600KG
Warhead: 87Kg HE
Propulsion: Ramjet + integral solid rocket boosters
Max speed: Mach 4.5
Max effective range: 110km
Guidance: L-112E passive radar homing, D~F band

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By: Sintra - 24th August 2015 at 18:33

We either do the same as the French & send off a general-purpose PGM (preferably with an imaging seeker) towards the identified location of a SAM system, or hurriedly buy something from someone else if we ever need it.

That MBDA Spear III thingy might have something to do with the RAF decision of not acquiring a direct follow on (AKA “anti radar specialist munition”) replacement for ALARM (that or i am being too optimist and the actual answer is “no money”).

Cheers

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By: bring_it_on - 23rd August 2015 at 13:50

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By: swerve - 14th August 2015 at 11:10

Despite saying that the missile was retired almost two years ago.

Looks as if either it was worked out that they’re not all time-expired & they’ve not all been thrown away, or someone’s been replacing the propellant & anything else that’s too old.

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By: mrmalaya - 13th August 2015 at 18:30

See the post I made in the missile news thread.

The RAF are still training to use the ALARM on GR4s.

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By: swerve - 13th August 2015 at 14:38

IIRC the missiles in stock were reaching the end of their lives, & neither re-starting production nor refurbishing the existing stock was thought worth paying for. We either do the same as the French & send off a general-purpose PGM (preferably with an imaging seeker) towards the identified location of a SAM system, or hurriedly buy something from someone else if we ever need it.

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By: RacingMonk - 13th August 2015 at 08:58

Why did the RAF get rid of ALARM? Was it rubbish? It seemed on paper to be a very clever system and leaves an obvious gap in capabilities. Do they just plan to throw Storm Shadows at SAM sites from now on?

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By: TR1 - 5th August 2015 at 22:42

With a bit of help from the editor of ‘Jane’s Air-Launched Weapons’, and from the Imperial War Museum, I have tracked down a definitive answer to the question of how the ALARM missile operates.

Following the 1999 Gulf War, Bob Bartlett, at that time the programme manager for ALARM at BAe Stevenage, gave an interview to the Swiss aviation magazine ‘Interavia/Aerospace World’, and described how the missile works. The single-burn motor has conventional boost and sustain phases, and the missile’s diving attack is unpowered.

The published version of the article was heavily edited to reduce its length, but yesterday I saw a draft of the original text. This contains a lot of fascinating material that it is still unpublished. (If I may paraphrase the style of the late Dr John Watson of 221b Baker Street, ‘The Case of the Terrified Secretary’ has yet to be placed before the public.)

Given that the missile must be coming to the end of its service life, I wondered if the IWM already had an ALARM in its collection. I checked, and it has. The museum’s notes on the missile state “Once the target has been acquired, the missile releases the parachute and falls under gravity to the target.”

So there we have it – the missile behaves just as I had described.

Bayern Chemie was right.

Jane’s was right.

The Federation of American Scientists was right.

Mercurius was right.

The Wikipedia entry for ALARM was wrong.

The Flight International news story that the Wikipedia entry had cited was wrong.

Lukos was wrong.

I did my best to explain the missile’s operating principles back in mid-November, but Lukos preferred to expound his own opinions. Despite his determination to defend these in the face of evidence to the contrary, his opinions are now shown to be completely wrong (and about as valid as his criticism of my analytical skills).

I suppose that he could try to argue that the ALARM programme manager was a mere undergraduate or even a work experience student (just like those chaps at Bayern Chemie), or perhaps that the man was so senior that he did not understand how his own missile worked. But as far as I am concerned, the programme manager is about the most reputable source you can ask for.

Case closed.

Sorry for ridiculous bump – but great info, thanks Mercurius.

Meanwhile, the myth continues:

https://en.wikipedia.org/wiki/ALARM

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By: blackadam - 3rd March 2015 at 22:58

Su-25, Su-34 has also been successfully used Kh-31P and Kh-25, to disable enemy air defense forces in Kuwait, Iran and Georgia

I did not find any statistically significant achievements of HARM, positive as the air defense system of Iraq and Yugoslavia were paralyzed by rain bombs from F117, B2 and Tomahawk not by HARM

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By: sheytanelkebir - 16th December 2013 at 09:58

great result! another myth laid to rest.

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By: Mercurius - 15th December 2013 at 21:10

I cannot speak for engineering students, but this thread it is a good illustration for the forum in general of the problems created by over-reliance on questionable data.

A common part of any discussion here is the demand for ‘links’. To some people, ‘links’ = proof.

But what we had here was an instance where some websites said one thing, and some said another. Since both could not be right, it was a matter to trying to find which was likely to be the more reliable.

Unfortunately, the skills needed to analyse evidence are not too strong on most aviation fora. It often boils down to “a source that agrees with my beliefs is right; one that disagrees with my beliefs must be wrong”. I think this principle was being used by Lukos when he dismissed information published by the motor manufacturer as perhaps being the work of undergraduates or even work-experience students.

The situation with ALARM soon escalated ‘behind the scenes’, since Jane’s needed to know whether its description of the missile in ‘Jane’s Air Launched Weapons’ was correct. So finding an answer has involved a significant amount of work for several individuals over a period of several weeks.

But we got there, and the myths of a second motor burn or the existence of a secondary rocket motor can now be laid to rest.

So Jane’s can refine its ALARM description, and anyone who researches this subject in future will be able to find this thread.

The only correction I would make to what I wrote earlier in this thread is that since an ALARM round recovered by the Serbs shows only a single efflux pipe, the “twin nozzle arrangement” (Doppeldüse) described by Bayern Chemie may not have been of the concentric form I had suggested from what I remembered from photos of the Serbian example seen more than a decade ago.

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By: Arabella-Cox - 14th December 2013 at 19:09

With a bit of help from the editor of ‘Jane’s Air-Launched Weapons’, and from the Imperial War Museum, I have tracked down a definitive answer to the question of how the ALARM missile operates.

Following the 1999 Gulf War, Bob Bartlett, at that time the programme manager for ALARM at BAe Stevenage, gave an interview to the Swiss aviation magazine ‘Interavia/Aerospace World’, and described how the missile works. The single-burn motor has conventional boost and sustain phases, and the missile’s diving attack is unpowered.

The published version of the article was heavily edited to reduce its length, but yesterday I saw a draft of the original text. This contains a lot of fascinating material that it is still unpublished. (If I may paraphrase the style of the late Dr John Watson of 221b Baker Street, ‘The Case of the Terrified Secretary’ has yet to be placed before the public.)

Given that the missile must be coming to the end of its service life, I wondered if the IWM already had an ALARM in its collection. I checked, and it has. The museum’s notes on the missile state “Once the target has been acquired, the missile releases the parachute and falls under gravity to the target.”

So there we have it – the missile behaves just as I had described.

Bayern Chemie was right.

Jane’s was right.

The Federation of American Scientists was right.

Mercurius was right.

The Wikipedia entry for ALARM was wrong.

The Flight International news story that the Wikipedia entry had cited was wrong.

Lukos was wrong.

I did my best to explain the missile’s operating principles back in mid-November, but Lukos preferred to expound his own opinions. Despite his determination to defend these in the face of evidence to the contrary, his opinions are now shown to be completely wrong (and about as valid as his criticism of my analytical skills).

I suppose that he could try to argue that the ALARM programme manager was a mere undergraduate or even a work experience student (just like those chaps at Bayern Chemie), or perhaps that the man was so senior that he did not understand how his own missile worked. But as far as I am concerned, the programme manager is about the most reputable source you can ask for.

Case closed.

Very interesting dialog…good story for engineering students.

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By: Mercurius - 13th December 2013 at 14:23

With a bit of help from the editor of ‘Jane’s Air-Launched Weapons’, and from the Imperial War Museum, I have tracked down a definitive answer to the question of how the ALARM missile operates.

Following the 1999 Gulf War, Bob Bartlett, at that time the programme manager for ALARM at BAe Stevenage, gave an interview to the Swiss aviation magazine ‘Interavia/Aerospace World’, and described how the missile works. The single-burn motor has conventional boost and sustain phases, and the missile’s diving attack is unpowered.

The published version of the article was heavily edited to reduce its length, but yesterday I saw a draft of the original text. This contains a lot of fascinating material that it is still unpublished. (If I may paraphrase the style of the late Dr John Watson of 221b Baker Street, ‘The Case of the Terrified Secretary’ has yet to be placed before the public.)

Given that the missile must be coming to the end of its service life, I wondered if the IWM already had an ALARM in its collection. I checked, and it has. The museum’s notes on the missile state “Once the target has been acquired, the missile releases the parachute and falls under gravity to the target.”

So there we have it – the missile behaves just as I had described.

Bayern Chemie was right.

Jane’s was right.

The Federation of American Scientists was right.

Mercurius was right.

The Wikipedia entry for ALARM was wrong.

The Flight International news story that the Wikipedia entry had cited was wrong.

Lukos was wrong.

I did my best to explain the missile’s operating principles back in mid-November, but Lukos preferred to expound his own opinions. Despite his determination to defend these in the face of evidence to the contrary, his opinions are now shown to be completely wrong (and about as valid as his criticism of my analytical skills).

I suppose that he could try to argue that the ALARM programme manager was a mere undergraduate or even a work experience student (just like those chaps at Bayern Chemie), or perhaps that the man was so senior that he did not understand how his own missile worked. But as far as I am concerned, the programme manager is about the most reputable source you can ask for.

Case closed.

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By: mrmalaya - 26th November 2013 at 13:19

Funny, but in my experience on this forum its the engineers who enjoy rubbing people up the wrong way and have to be right all the time. I have one particular 1990s vintage computer in mind but there are others and lukos I can’t see what you are getting out of this exchange now…

And I don’t see what else there is to gain by showing us pictures of you doing the ironing…..:angel:

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By: lukos - 24th November 2013 at 20:36

The feeling is mutual, I assure you.

And just for the record, anyone who writes factual material for a living is by definition either a primary, secondary, or tertiary source. There is no level below tertiary. Most of my writing is secondary source material, with the odd bit of primary to the degree that the provisions of the Official Secrets Act allows.

I only write primary source material for a living because I’m an engineer. Given your analysis on range, probably best if you stop writing primary source material altogether.

So that makes it a secondary source, just like all the other defence magazines. The only thing ‘special’ about it is that it is widely trusted by knowledgeable insiders in industry and elsewhere.

Who can’t disclose any more than the OSA allows them to, so really nothing ‘special’ at all, they get their water from the same well as everyone else in that field.

Whenever I read that “everyone knows…” I confidently assume that I am about to read BS.

In this case, it is clear that you cannot perceive the difference between a weapon that loses height during its flight to the target, and one whose mission requires it to maintain height.

http://2.bp.blogspot.com/-xVStZRWvK5g/TfpWYPA2URI/AAAAAAAADGw/7fc5Cv0P978/s400/man-ironing.jpg#man%20ironing

I have done my best to try to explain how Alarm works, but if you wish to believe an alternate theory, then be my guest.

Consider me your guest.

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By: Mercurius - 24th November 2013 at 19:24

Well guess what? You aren’t a primary, secondary or tertiary source and I don’t care what you think..

The feeling is mutual, I assure you.

And just for the record, anyone who writes factual material for a living is by definition either a primary, secondary, or tertiary source. There is no level below tertiary. Most of my writing is secondary source material, with the odd bit of primary to the degree that the provisions of the Official Secrets Act allows.

Jane’s is also, at best, a secondary source despite the credence people place in it. It gets its information from similar sources to every other military magazine.

So that makes it a secondary source, just like all the other defence magazines. The only thing ‘special’ about it is that it is widely trusted by knowledgeable insiders in industry and elsewhere.

Ranges? You’re kidding me right? Everyone knows….

Whenever I read that “everyone knows…” I confidently assume that I am about to read BS.

In this case, it is clear that you cannot perceive the difference between a weapon that loses height during its flight to the target, and one whose mission requires it to maintain height.

I have done my best to try to explain how Alarm works, but if you wish to believe an alternate theory, then be my guest.

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By: lukos - 24th November 2013 at 16:21

I am not sure that Wikipedia constitutes a ‘reputable source’! It is at best a secondary source, and more often a tertiary source. Nor do I think that Flight had any missile specialists on their staff when that late 1980s news report you cited was written.

Well guess what? You aren’t a primary, secondary or tertiary source and I don’t care what you think.

Jane’s is also, at best, a secondary source despite the credence people place in it. It gets its information from similar sources to every other military magazine, or simply reprints press releases from elsewhere, so no, there’s nothing special about it and I don’t see a link. The undergraduates point is also an absolute fact. I see incorrect stuff on BAE’s site all the time as a result of it.

Ranges? You’re kidding me right? Everyone knows range is a hairy-fairy figure, heavily dependent on launch altitude, speed and trajectory. An SDB has no motor at all and still manages a range of over 100km, even a 1,000lb JDAM brick can manage 45km with a supersonic launch. Last I heard the latest MLRS developments were aimed at lobbing 90kg warheads 120km with 4m-long, 227mm-diameter rockets with far less aerodynamic surface area. I don’t even know what your 45km figure refers to? Confusing Skyflash with ALARM perhaps? Oh well, there goes your attempt at an analysis. Good day.

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By: Mercurius - 23rd November 2013 at 17:45

I am not sure that Wikipedia constitutes a ‘reputable source’! It is at best a secondary source, and more often a tertiary source. Nor do I think that Flight had any missile specialists on their staff when that late 1980s news report you cited was written. In the 1960s and 1970s, the magazine employed at different times Gunston, Hewish, and Richardson, but when the last of these left the magazine, he was kept under contract to write their annual missile surveys and some of their major missile articles. So there must remain a possibility that an inexperienced reporter got it wrong, and that his error was picked up by other secondary and tertiary sources.

Let us consult the reference book ‘Jane’s Air Launched Weapons’. What does it say?

“The ALARM has a solid-propellant dual chamber, boost and sustainer motor. This gives the missile a range of about 45 km when launched from high altitude.”

It elaborates:
“In direct, dual or loiter modes, following launch, the ALARM climbs to altitude and coasts towards the target area.”

So how does Alarm coast for tens of kilometres without sustainer power? You will not get 45 km range or more from just a boost burn. A weapon with a short burn would have a range of less than 10 km. The Genie air-to-air missile could only manage around 10 km at altitude.

A look at the specification of heavy air-to-surface rockets will show ranges of only a few km. So that sustainer burn is needed to provide Alarm’s coasting range.

Describing the loitering mode under the parachute, Jane’s states:

“If a target is detected, then the parachute is jettisoned and the missile dives down onto the target.”
There is no mention of this dive being under power.

I have a reasonable experience of both receiving and giving briefings, so you can be assured that Alarm’s mission and operating modes were explored in some detail during my early 1990s briefing. I no longer have my notes from this, while the computer file containing my subsequent report is now missing a major part due to a computer problem. But both would have still been available for consultation several years later when I wrote a more general report on anti-radiation missiles. That text described how after releasing its parachute, the Alarm missile makes an unpowered dive on the target. So it is reasonable to assume that this reflects what BAe Dynamics had told me.

It is not particularly useful to dismiss facts that do not support your opinion as perhaps having come from “undergraduates and even work experience students”. I do spend a lot of time at air shows visiting stands and chalets and talking with the company engineers, and my office is a near-impassable maze of boxes containing the technical literature I have gathered.

The high degree of motor turn-down reported by Bayern Chemie is well-matched to the task of proving high-altitude cruise power, but not the task of powering a final descent phase. Since target-detection could come at a relatively late stage of the parachute descent, a short burn time would be more desirable for such a late burn.

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By: lukos - 23rd November 2013 at 14:02

So you have the choice of believing Flight (which by the late 1980s was a shadow of what it had been in the days when Gunston and Hewish did their missile reporting), or of believing the company that manufactures the rocket motor in question.

I’ll put my money on what Bayern Chemie statement – a single-pulse boost/sustain motor.

Also, I had a long briefing on Alarm soon after its combat debut, and the manufacturer made no claim of a second delayable burn.

What has probably confused some people is that the motor has two concentric nozzles – one optimised for the boost phase and the other for the sustainer phase. The reason for this arrangement is that the motor was required to deliver a level of sustain thrust that was very much lower than the boost thrust. This turn-down ratio was probably pushing the state of the art at the time the motor was designed.

Or maybe you are just plain wrong about everything and its motor can be stopped and started exactly as my Flightglobal link states along with the original link I posted to the article in Wikipedia.

Company websites are often done by undergraduates and even work experience students, so don’t place too much trust in them having all their facts straight, especially when you have 2 reputable sources to the contrary. All discussions I’ve had with people inside MBDA suggest burn-stop-burn operation.

Also – don’t confuse the absence of a claim with a claim to the contrary. Commonsense should also tell you that in such a time-critical situation free-fall would be less effective.

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By: Mercurius - 22nd November 2013 at 20:59

So you have the choice of believing Flight (which by the late 1980s was a shadow of what it had been in the days when Gunston and Hewish did their missile reporting), or of believing the company that manufactures the rocket motor in question.

I’ll put my money on what Bayern Chemie statement – a single-pulse boost/sustain motor.

Also, I had a long briefing on Alarm soon after its combat debut, and the manufacturer made no claim of a second delayable burn.

What has probably confused some people is that the motor has two concentric nozzles – one optimised for the boost phase and the other for the sustainer phase. The reason for this arrangement is that the motor was required to deliver a level of sustain thrust that was very much lower than the boost thrust. This turn-down ratio was probably pushing the state of the art at the time the motor was designed.

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By: lukos - 17th November 2013 at 14:45

You’re incorrect in your assertions regarding post loiter operation.

http://www.flightglobal.com/pdfarchive/view/1987/1987%20-%201575.html

Once a target has been
acquired the parachute is
jettisoned and the motor
restarts, boosting the missile
to its target.

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