Iran military downs US RQ-170 Sentinel spy drone

'Dear Pakistan - all your airspace belong are to us!'

'Dear Iran - bbwwhahahahaha'

A very nice turn out and it will be very interesting to say the least to see if this is followed by its stretched and heavier armed brethren.
 
a other US Drone has crash
"MQ-9 Reaper" just impact on runway of international airport, of Mahé.
The main island of the Seychellen,
the MQ-9 try to land after a mission (to spy on Somalia pirates ?)
Source in german
http://www.spiegel.de/politik/ausland/0,1518,803549,00.html
 
Trident said:
Well, if you were agreeing with what bipa said there, responding with what amounts to "No, you're wrong" when taken at face value seems like a patently unhelpful way of expressing your agreement.

I wasn't agreeing at all, I was pointing out that the explanation given applies to scale model testing, because the frequency is scaled. RCS itself is a measure of power the target reflects back at the radar - this is why it's typically expressed as dBsm. The dBsm is expressed as -20dBsm, etc. -20? Well, 20 less than what?
20 less than a (theoretical) perfectly conducting metal sphere at least several wavelengths in diameter. A sphere reflects in all directions equally for all viewing aspects. To calibrate a radar (or RCS test), a sphere is used for just these reasons. Once calibrated, you have the numbers for your ideal sphere - which removes frequency from the process (this is why the ideal sphere is x wavelengths in diameter).

The idea that RCS is dependent on the "size/frequency ratio" is not accurate, because RCS itself has no frequency component. As stated above, frequency is removed on purpose. When testing a scaled model though, frequency is a factor because those several wavelengths for the idea sphere have to be scaled as well.
So RCS itself has no frequency, and is not affected by scale. Scaled model RCS testing does, because the whole point is to scale the results to a real world object.

Ian33 said:
Tape?

So an LO airframe flies about for years with two strips of uncovered tape? And not into undefended airspace but highly defended as well?

Do LM not have a repairs facility? is this tape so supreme that it can replace LO skin on such a vulnerable area? I am skeptical to say the very least.

It's likely that like the tape holding the wings in place, this was applied by the new owners.
 

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@ Quellish. That makes perfect sense now you say it.
RQ goes in soft but still takes a beating and the Iranians use the 'black nasty' to make it look more acceptable and complete (as if they flew it in not that it glided and pancaked in sheer naked bad luck).

I'll accept that and go hide back in my hobbit hole.
 
sealordlawrence said:
http://www.defensenews.com/story.php?i=8530940&&s=TOP


My favourite is this from Mohammad Khazaee, apparently waiting for a subsonic aircraft to fly 150 miles into your airspace before shooting it down is "timely":


"After reaching the northern part of Tabas area - 150 miles deep inside Iranian territory - the aircraft was confronted by the timely response of the Islamic republic's armed forces,"

Not to mention that is is an aicraft that is designed to fly at about 300 miles per hour max, and which would have been loitering for some time above it's target area. The kind of aircraft that would be very easy to shoot down with small arms fire if you have a visual and if it was flying relatively low (it does not appear to be designed to fly as high as Global Hawk and the U-2, with its small short wings).

Did anyone notice that there are at least 2 fist size impact damage marks on the leading edge in the video ? (that and the 'taped' wing). Seems to me that this bird didn't go down because it had it's comlink hacked (either that or the Iranians kicked it). Though the possibility that the Iranians took control of the UAV in mid-air is not impossible, remember there was a group of hackers that took control of a UK spy satellite a few years ago.. My own suspicion is that if this is the case here again, they might have received some outside help to do so, say from a super-power who wants to continue to sell them weapons..
 
Flight control systems and autopilots are two different things. The F-16 needs it's flight control system to remain stable, because it was designed to be statically unstable. It does not need an autopilot. There is no reason to think that the RQ-170 is not statically stable - it may naturally return to wings level flight without help from the flight control system to maintain stability.



From what i remember reading the Horten flying wing sailplane were difficult to land, one or more of them were damaged or crashed after the war, and those were the days before SAS flight control systems. Very few people knew how to fly and land the Horten well, like the Horten flight test pilot for exemple (if not the only guy who could do it without damage).
 
quellish said:
The idea that RCS is dependent on the "size/frequency ratio" is not accurate, because RCS itself has no frequency component. As stated above, frequency is removed on purpose. When testing a scaled model though, frequency is a factor because those several wavelengths for the idea sphere have to be scaled as well.
So RCS itself has no frequency, and is not affected by scale. Scaled model RCS testing does, because the whole point is to scale the results to a real world object.

You are right that the RCS measurement when done like this has no frequency component. However, the amount of radar energy returned by an aircraft can vary with the radar frequency: smaller features on the aircraft can be as large as the radar wavelenght, and then your 'diameter of the sphere is several wavelengths' assumption goes out the window. Also radar absorbing materials work better at some wavelengths than others.
 
Gents,

Those black strips near the nose of the aircraft were certainly not added by the Iranians..Since those strips are visible in the 2009 images of the Sentinel on the runway! What purpose those strips serve IDK but they were not something the Iranians put on the drone.
 

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Eagle2009 said:
Gents,

Those black strips near the nose of the aircraft were certainly not added by the Iranians..Since those strips are visible in the 2009 images of the Sentinel on the runway! What purpose those strips serve IDK but they were not something the Iranians put on the drone.

Those do look like narrow windows to me.
 
I would agree with that, being that there are no visible pitot tubes, and Lockheed had worked on that laser system for the air data computer.
 
V-Indicator?. I Laughed when the penny dropped. Then I see why the USAF wanted that craft bombed to small pieces or picked up by SOF troopers.

Not something you'd want the Chinese seeIng up close.
 
I know this might be a long shot, but does anyone by any chance have any photos of the A-12 Avenger IIs LPI SAR?
 
I think there's many more descriptive words that could be used than "hijacking", from "jamming" to "cracking". Wish they'd be more precise...


I wonder if the -170 has a thumb drive slot?
 
Gridlock said:
I think there's many more descriptive words that could be used than "hijacking", from "jamming" to "cracking". Wish they'd be more precise...


I wonder if the -170 has a thumb drive slot?

"Spoofing" would more accurately describe what is discussed in the article. The one thing the source said that is consistent with real world spoofing against a UAV or missile is the altitude, and this is consistent with where the vehicle came to a rest (the elevation is about right vs. OAKN). Ground photos do not show a controlled landing, but could be consistent with spoofing to a landing.
 
http://security.blogs.cnn.com/2011/12/15/crashed-drone-was-looking-at-iran-nuclear-sites/?hpt=hp_t2
Crashed drone was looking at Iran nuclear sites
The Sentinel drone that crashed in Iran last week was on a surveillance mission of suspected nuclear sites in the country, U.S. military officials tell CNN.

Previously, U.S. and NATO officials had said the drone was on a mission to patrol the Afghan-Iran border and had veered off course.

The officials say the Afghan government was unaware of the use of its territory to fly surveillance drones over Iran, and that the CIA had not informed the Defense Department of the drone's mission when reports first emerged that it had crashed. One official told CNN that the U.S. military "did not have a good understanding of what was going on because it was a CIA mission."
 
Thats career suicide lying to the 5 Stars. They lie to the POTUS and Sec Def, and the sh*t you rolled uphill just snowballs on its way back down and wipes you out.

Lob up a turd, coming down is a sh*t avalanche filled with rocks and anything else they want to throw. Hung. To. Dry.

Also says to me that this Iranian toy is indeed the pre production 2002/2003 beast used over Iraq by the CIA and not the full size ful scale deep grey / light grey vehicle flown for the USAF by the USAF.
 
If the asset was spoofed, I find it hard to believe the Iranians accomplished it all on their very own--most likely there was significant technical assistance from Russian signal intelligence specialists. The Russians are not idiots. They fully recognize the stategic implications of US drone hegemony. Furthermore, a large Russian cohort of signal intelligence types have been operating against us in Iraq from the very beginning–day one. This operation has GRU written all over it.

Bronc
 
Broncazonk said:
The Russians are not idiots. ... This operation has GRU written all over it.

Maybe. But if so, I imagine right now they're *pissed.* They showed their hand on what was essentially a trivial mission. If you have the technology to knock drones out of the sky, you don;t tell the world you have it; you wait until your skies are swarming with them.
 
GPS spoofing is technically much harder than jamming, but doesn't take that much expertise. A US academic has demonstrated his own GPS spoofer, and the Iranians have plenty of resources.
It helps that the Sentinel has no situational awareness and wouldn't react to a jamming/spoofing aircraft flying alongside it.
 
All of the above, and more, of course. But mostly "analysts" and "sources" escalating their worth with nods and winks and hints of inside access for the official court press.


I'm confident Obama asked Iran for a drone back, anything else is pretty much suspect information really. The wind turbine software is cool though.
 
Correct me if I am wrong, but the unamed source in the article mentions there's something wrong with the WELDS of the aircraft shown..Except this aircraft is built from COMPOSITES which would mean there shouldn't be any visible welds at all right?

Further, did anyone else notice the specifications the article gives for the Sentinel are even BIGGER than the numbers provided by Iran? The article claims a wingspan of 27.43 meters compared to the 26 meters claimed by Iran, and apparently the article's figure comes from Airforce-technology.com. Considering how specific the figure is, maybe the analysis I posted earlier about the Sentinel being much smaller than reported is wrong after all..
 
quellish said:
Trident said:
Well, if you were agreeing with what bipa said there, responding with what amounts to "No, you're wrong" when taken at face value seems like a patently unhelpful way of expressing your agreement.

I wasn't agreeing at all, I was pointing out that the explanation given applies to scale model testing, because the frequency is scaled. RCS itself is a measure of power the target reflects back at the radar - this is why it's typically expressed as dBsm. The dBsm is expressed as -20dBsm, etc. -20? Well, 20 less than what?
20 less than a (theoretical) perfectly conducting metal sphere at least several wavelengths in diameter. A sphere reflects in all directions equally for all viewing aspects. To calibrate a radar (or RCS test), a sphere is used for just these reasons. Once calibrated, you have the numbers for your ideal sphere - which removes frequency from the process (this is why the ideal sphere is x wavelengths in diameter).

The dBsm scale is relative to 1 square meter (ie zero dBsm). While the RCS of a sphere indeed becomes independent of frequency in the high-frequency regime, I don't see how this fact "removes frequency from the process". Actually it just removes it in the case of a sphere (or ellipsoid).

Maybe you were awkwardly referring to expressing RCS in "lambda squared" or "dB_lambda_squared" (lambda == wavelength), which is often used in theoretical literature to keep only the size/wavelength dependence and remove the dependence versus frequency alone. Indeed, the corollary of the "RCS scaling property" (as expressed in my previous post) is that RCS, when expressed in "lambda squared" instead of square meters, depends only on the size/wavelength ratio.

But in the real world, when you are facing an actual radar, only the square meter / dBsm scale counts, so the frequency dependence will re-appear: namely in the case of downscaled objects at downscaled wavelength, the RCS in square meters will also be downscaled (by the square of the scale, just like "lambda squared").

So I dare to insist: speaking in dBsm, the downscaled (bird sized) B-2 model at the upscaled frequency should have a much lower RCS than the actual B-2 at the actual frequency (and not the exact same RCS as you seemed to claim).

quellish said:
The idea that RCS is dependent on the "size/frequency ratio" is not accurate, because RCS itself has no frequency component. As stated above, frequency is removed on purpose. When testing a scaled model though, frequency is a factor because those several wavelengths for the idea sphere have to be scaled as well.
So RCS itself has no frequency, and is not affected by scale. Scaled model RCS testing does, because the whole point is to scale the results to a real world object.

I have never said that RCS depends on "size / frequency" ratio. Rather I have said that absolute RCS magnitude of an object (in square meters) depends on frequency and on the "size / wavelength" ratio (please re-read my previous posts carefully). In other words, that means it depends on frequency and on the "size x frequency" product.

Given that and all of the above, I really don't understand how you can conclude that:

quellish said:
RCS itself has no frequency, and is not affected by scale

because physics works in the exact opposite way... IMO you should clarify what you meant with this sentence.
 
every DoD or MoD has its own retired idiots
http://www.usatoday.com/news/world/story/2011-12-14/iran-drone-united-states-spy-plane/51936376/1
 
I was wondering about this scenario -

CIA Drone over significant target. Just about to turn tail and go home when it gets an urgent tasking.

Urgent tasking takes it into dangerously low fuel levels. Route home too far after looking at fuel, so operator flies it as far into a remote mountainous area for SOFD-D retrival team to go fetch.

Fuel just about gone, the pilots trim it intentionally for a glide profile and 'fly' it as far as it can go, then engine out, coasted in. Hence lack of damage.

CIA know where it is but POTUS vetos retrival. CIA screwed the pooch, and Iran gets a drone via tribes people who saw the drop in location.

No jamming, no GPS spoof, just a plain good old FUBAR.
 
Interesting piece about where this thing probably came from historically.
http://aviationintel.com/?p=4873
Cool theory on the re-tasking idea.
 
Eagle2009 said:
Gents,


I recently ran into something interesting on Wikipedia's page of the RQ-170, namely in the Discussion section. IN said section, an author makes the argument that one of the stated dimensions for the Sentinel is WAY off, while the other two are fairly accurate. He/she did so by imagery analysis and I think they make an interesting argument.


He/she also includes an image that helps to illustrate the issue he is raising, here is the link to the discussion page:
http://en.wikipedia.org/wiki/Talk:Lockheed_Martin_RQ-170_Sentinel#Specifications.


Thoughts?


I'm re-posting some geometric sizing analysis I ran on the Michael Yon image - in December 2010 - on another forum. I tend to believe the RQ-170 is smaller than we've been hearing. The following analysis supports that posted in the Wikipedia discussion above.


Michael Yon Image Photogrammetry Estimate
-----------------------------------------

I looked into the Michael Yon image a little further and noticed the holding position sign labeled "5-23" in the background, just aft of the port wingtip of the RQ-170. I looked into signage specs online and found the following link:

Planning and Design of Airports by Robert Horonjeff - Page 338

The table states the sign legend (i.e. inscription) can be 15 to 18 inches in height, depending on the "effectiveness, aircraft clearance, jet blast and snow removal" (per the referenced book). We can assume, since the sign is behind the RQ-170, it can be used as a reasonable scale to measure the distances on the airframe.

If the distance from the camera to the RQ-170 is much greater than from the RQ-170 to the sign, then it is reasonable and can be proven with a little geometric analysis. In reality, the aircraft will measure smaller than if the signage height is used as the measuring unit. Also, per the link below, a standard taxiway light stands 14 in:

GSI-LED-861-T

I downloaded the original Michael Yon image from flickr:
Michael Yon Image

Then overlaid it in MS PowerPoint and, leaving the original aspect ratio alone, resized it at 9.0 in by 6.0 in. I overlaid a rectangular shape and found the holding position sign font to be 0.095 in (it is to be at least 15 in tall, per the book). I also found the taxiway light in the near field to measure 0.48 in (it is 14 in per the GSI link). This allowed me to measure the RQ-170:

Height = 0.60 in
Tip to Tip = 3.96 in
Starboard = 0.82 in
Port = 3.14 in

So drawing lines from the near to the far field heights of 14 inches, and pick 2/3 of the way from the taxiway light to the holding position sign, we get a scale of about 82:1 for an image that is 9.0 in by 6.0 in.

Height = 49.4 in = 4.1 ft
Tip to Tip = 325.9 in = 27.2 ft (at this offset angle we are looking from)
Starboard = 67.5 in = 5.6 ft
Port = 258.4 in = 21.5 ft

I also ran a cosine table (of offset angle) of estimated wing spans, varying the offset angle we are viewing the RQ-170 off it's centerline. As a result, I'm estimating the following wing spans:

View Angle [deg] = Wing Span [ft]
30 deg = 31.4 ft
45 deg = 38.4 ft
60 deg = 54.3 ft

My best estimate is that we're viewing a little more than 45 deg, but less than 60 deg, putting the wing span at around 46 ft. I believe Bill Sweetman's estimates are over 75 ft, however I tend to agree with Astr0 and believe it is significantly smaller than first thought.

Another element to consider is they're likely running a Williams International FJ-44-X core turbofan and these engines are not that powerful, thus supporting the smaller airframe theory. If you look at the FJ-44-4, the thrust rating for an uninstalled single engine runs 3,600 lb. With a fairly conservative T/W ratio of 0.35 and an inlet installation loss of 25% (you'll likely see more due to the grid inlet and extreme flow turning angle at higher total AoA), you get a TOGW around 7,700 lb which is small. RQ-3A TOGW was 8,500 lb.
 
Aviation Week has some good photos of the drone in flight, and you can see the sensor turret behind plated glass on the bottom of the vehicle.
 
People have been commenting on the "strange" LO (?) camo on the drone (at least because it's not grey like in the original airfield images). There's an article on io9 about some WW2 "spy" planes (Spitfires in this case) being painted sorta dirty pink - something that to me is reminiscent of the RQ-170 in the iranian pictures (... the pink scheme also discussed here by Michael Van and others). Apparently there are good optical reasons to do this, especially in morning/evening conditions. The hue in the pictures might even be a little bit off from the intended outdoor effect due to artificial lighting and all the scattering from wooden and painted surfaces.

In other news the Shindand airfield in Afghanistan is being noted in a new Defensetech blog entry, because of its proximity to Iran and also drone operations.
 
blackstar said:
Aviation Week has some good photos of the drone in flight, and you can see the sensor turret behind plated glass on the bottom of the vehicle.

Hard copy magazine or web based? If you have a link it would be appreciated.

*Interesting to see a more Irancentric airfield in the spotlight.
 
Ian33 said:
blackstar said:
Aviation Week has some good photos of the drone in flight, and you can see the sensor turret behind plated glass on the bottom of the vehicle.

Hard copy magazine or web based? If you have a link it would be appreciated.

*Interesting to see a more Irancentric airfield in the spotlight.

I have the paper copy, but they keep most of their articles behind a firewall. I have not looked to see if this is on their main site.

I read the article. Sweetman is one of the authors, so it's not baloney. But it doesn't appear to include anything that could be considered insider data. The most notable thing it says is quoting a low-observable expert who says that this is a standard turret ball behind a L/O facet. Also refers to this as essentially a "sensor truck" and not an exotic L/O design. It's simply supposed to do basic things, but be less observable than a Predator. Also notes that with the high loss rate for Predator, nobody should be surprised that they lost an RQ-170. (I think the implication is that everybody involved in building this aircraft knew that at some point it would crash behind lines.)

Also notes that the turret ball is relatively low below the fuselage, so a belly impact would have crushed it and caused a lot of damage. I presume that is why the Iranians covered that up, because they didn't want the US to know how much had been recovered.

I'm not totally sure I buy that. It seems possible that although the ball might have been smashed a bit and shoved up into the fuselage, somebody still could have pieced it back together. Just that impact damage is not going to break it into tiny pieces. Now where were the control electronics? In the ball or in the fuselage and better protected? And did it have any kind of memory system that could be retrieve? If it was simply full motion video, it might have not recorded anything onboard but sent it all up through the comm, therefore not leaving any sensor data on board. (That said, I presume a big issue would be any recorded commands or GPS data. You would not want the Iranians to recover the flight path.)
 
You can't have it both ways; if this is an airframe that everybody expected to lose behind the lines sooner or later then you can be sure that one area it probably is state of the art in is secure controlled destruction or whatever the TLA is.


Think back to Pueblo and the Chinese spy plane contretemps and you can see that equipment and data destruction is Job 1 when you no longer 'own' the asset. The inside of this thing probably looks like a decade-old barbecue pit.
 
Gridlock said:
You can't have it both ways; if this is an airframe that everybody expected to lose behind the lines sooner or later then you can be sure that one area it probably is state of the art in is secure controlled destruction or whatever the TLA is.


Think back to Pueblo and the Chinese spy plane contretemps and you can see that equipment and data destruction is Job 1 when you no longer 'own' the asset. The inside of this thing probably looks like a decade-old barbecue pit.

Well... yeah, but...

The airframe looked like it was essentially intact. You'd think that they would have equipped it with a destruct charge or something, right? And sometimes people just screw up. Remember that when Gary Powers got shot down, the CIA was certain that a) nobody could survive that, and b) the airframe would essentially disintegrate. They were wrong on both accounts.

I would like to think that the designers of the RQ-170 were incredibly smart people who figured out how to design the system so that as soon as the power went off, all the memory was erased. But we just don't know, and maybe we never will.
 
Gridlock said:
You can't have it both ways; if this is an airframe that everybody expected to lose behind the lines sooner or later then you can be sure that one area it probably is state of the art in is secure controlled destruction or whatever the TLA is.


Think back to Pueblo and the Chinese spy plane contretemps and you can see that equipment and data destruction is Job 1 when you no longer 'own' the asset. The inside of this thing probably looks like a decade-old barbecue pit.


You would hope, but then again I have it from two different sources that aircraft like that are supposed to also have a failure mode that causes them to auger straight down into the ground at high speed, and it did not happen
 
blackstar said:
The airframe looked like it was essentially intact. You'd think that they would have equipped it with a destruct charge or something, right?

Sure. But that destruct charge could easily be non-explosive, such as a gelled-acid or thermite charge to destroy vital/classified internal components, without (necessarily) doing external damage.

In fact, such a non-explosive destruct system makes sense (IMNSHO) for an aircraft intended to overfly inhabited territory (in case those 12 kg of C4 in the destruct package take out a school or a nursing home when they go BOOM).

Regards & all,

Thomas L. Nielsen
Luxembourg
 
blackstar said:
Gridlock said:
You can't have it both ways; if this is an airframe that everybody expected to lose behind the lines sooner or later then you can be sure that one area it probably is state of the art in is secure controlled destruction or whatever the TLA is.


Think back to Pueblo and the Chinese spy plane contretemps and you can see that equipment and data destruction is Job 1 when you no longer 'own' the asset. The inside of this thing probably looks like a decade-old barbecue pit.


I think that a destruct charge would be a very bad idea under any circumstances. If you were ground crew, would you want to handle anything that had a quantity of high explosives on board and which may or may not have a reliable fuse/detonator? One bad landing after a rough mission and you're lucky if you just have a crater in the runway. Pitching the nose down and throttling the engine up after a whole series of other programmed options have been tried first would be the logical solution.
 
MQ-9 doesn't have a destructor so how likely is that any other UAS will? To the best of my knowledge, very few aircraft do feature such a device (however IIRC, the dear old Vulcan did). The reasons for this are many and various but on an RPAS platform, you're generally tight for weight and space.
 

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