This type of aircraft RAM was first patented in 2008, I believe it to be the forerunner of the one destined for the T-50.
Its good to see you can tone your posts down from saying categorically that these materials will “definitely be used on component x on the pak fa” like you always have done in the past to “I believe” they will.
Sorry for offence, but the former really made your constant “hey there’s a new patent for PAK FA materials” posts seem like childish fantasy.
The mere presence of a patent accompanied with a general statement from the scientists such as “this could be used on aircraft” does not equate to “this material is a godsend, shaping is now obsolete and this is now used in the manufacture of the PAK FA’s inlet radar blocker”, I’m glad you realise this now like every other rational person.
In such scenario even mighty VLO fighter will suffer many loses
But still a whole lot less than any non-vlo platform. To say that a VLO airframe is not going to offer an advantage when it has been proven time and time again in real combat, exercises and by science, ignoring the fact that all major airforces are tripping over themselves to build or procure VLO and LO airframes, is pure delusion.
The RQ1 averaged around 0,06m^2 in RCS with a minimum RCS
What is your source for the RCS figures? With or without weapons, pylons, camera?
Too bad the Serbs didn’t know the ole SA-3 wasn’t a threat,
in spite of not being double digit and all that.
Would be interesting to know at what range the Serbs would have been able to engage the F-117 if they had longer range missiles. Probably would have only been 8 miles anyway, like the ones they hit with.
Running low frequency on the small aperture of the Sa-3 would have made the aperture’s directive gain absolutely woeful. Though they may have seen the F-117 coming a long way off, their beamwidth would have been too massive to be able to engage.
Being shot at by a battery 8 miles away is not so humiliating, even today’s stealth aircraft are designed to only be stealthy to SAM’s outside 30km or more. In the case of the PAK FA’s side aspect, roughly 190km according to APA, ie. fodder for anything on the network.
@ActionJackson :
Do you really believe that I ‘m gonna respond to someone calling me “flapping mouth” ? You are grossly mistaking .Apologize at once and I might change my mind .
Cheers .
Yeah that’s what I figured, knew you were just hot air. Time to find out if the ignore feature can remove all these spaces between the posts with substance.
The EW systems onboard the Eurocanards are miles ahead of the US fighters ‘s systems
In what way, exactly? Receiver counts, agility…etc. Give some detail so you don’t just look like the flapping mouth you come across as, or are uninsightful generalisations all you have? Sources…go.
Cannot comment on that, first time I hear this.. At least some data to support this stance would be good. I could imagine the idea of radar waves creeping along the fuselage but somehow miss the way of how could they be reflected back, then
Creeping waves can propogate along a surface until they reach a surface discontinuity or change in conductivity. Depending on the angle of the trailing edge relative to the leading edge, waves can reflect back off the trailing edge then scatter forwards from the leading edge (ie. the nose of the aircraft)
They also generate a large scatter at the trailing edge too.
Sawtoothing of trailing edges and panel joints in a manner consistent with the aircraft’s basic planform design prevents reflected running waves returning to the source radar.
Another method used is the application of small panels of surface ram with varying conductivity. The panels are also aligned in a similar manner to joints and edges. As surface waves hit each new panel of conductive ram, a small scatter of the running wave occurs. By breaking the waves into smaller scattered waves (and absorbing some at the same time), the overall return signal is much smaller and hidden within ambient noise.
US manufacturers really do a good job of reducing travelling waves. The image below shows the small conductive panels on the nose and body.
http://i.imgur.com/z26YqDd.jpg
Travelling waves are also the reason US don’t do exposed canopy frames on modern VLO fighters. Some people, ignorant of the subject matter, are quick to dismiss it as not required for no-compromise stealth maximisation, but they are absolutely and entirely incorrect.
Another question is how the F-35 fits in the equation with its roughly equally unstealthy rear end
Roughly equal in what way?
– There are no MiG-17s flying anymore in Cuba, the last ones were withdrawn from use as “trainers” in late 1980’s!
Better tell the IISS to pick up their game then.
EQUIPMENT BY TYPE
AIRCRAFT 45 combat capable (179 stored)
FTR/FGA 31: 2 MiG-29 Fulcrum; 1 MiG-29UB; 16 MiG-
23 ML Flogger; 4 MiG-23MF; 4 MiG-23UM; 4 MiG-21ML;
(in store: 2 MiG-29; 20 MiG-23BN; 4 MiG-23MF; 6 MiG-
23ML; 2 MiG-23UM; 70 MiG-21bis; 28 MiG-21PFM; 30
MiG-21F; 7 MiG-21UM; 4+ MiG-17; 6 MiG-15UTI)
According to them Egypt, Sudan, Tanzania, Bangladesh all flying J-6
Tanzania, North Korea are flying J-5’s
as of 2010…
Yeah, fox sort of describes the two interceptors. Unlikely to be used again for an aircraft with a totally different operational profile.
I was just looking up aircraft types and who has them for the “what’s the oldest combat aircraft in service thread” when I stumbled upon (the first time I’ve noticed it) the NATO naming conventions for Russian aircraft.
These forums don’t like their multiple threads per aircraft so didn’t start a new one. I thought it might be fun in here to take guesses at what the NATO reporting name of the PAK FA will be.
It’ll have to start with “F”, needs to sound a lot different to existing names over radio and NATO never gives cool names to russian aircraft (refer to the poor Ka-25 and Mig-15)
As its a reporting name that gets called when its first encountered, the obvious one that springs to mind for a stealth fighter is “Fu”
Anyone want to try their hand at playing Nostradamus, then come back in 5 years for bragging rights?
Using 2yo information and only fightery types and not taking into account combat:
Mig-15 (1947)
Cuba
Mig-17 (1952)
Cuba, Guinea, Guinea Bissau,
North Korea (J-5)
https://maps.google.com.au/maps?q=AFB,+North+Korea&hl=en&ll=38.900464,125.23372&spn=0.001785,0.004128&sll=40.369583,127.266532&sspn=0.001747,0.004128&t=h&hq=AFB,+North+Korea&z=19
Su-7 (1955)
North Korea
Hawker Hunter (1950)
Lebanon, Zimbabwe
Given a dull, overcast day I would highly doubt such shadow effects could result in such sharp, structured shapes on the port if it was a smooth, uniform surface a la ’51’ & ’52’.

I wouldn’t take any of that to the bank just yet.
Taking into account the direction of the sun, side-on and very slightly behind the aircraft and curvature of the APU inlet I say its more likely as follows (could be wrong, will certainly revisit it once better photos are available).
I believe the bottom dark area pointed to by label 1 in the pic above is the sun’s shadow of the small exhaust port at the top of the engine. The shadow is slight enlarged due to hitting a convex surface. This also checks out when looking at its placement on other prototypes. The top dark area pointed to by 1 is possibly the reflection of the same exhaust nozzle, or another shadow from a secondary light source (reflected ambient light off opposite stab). Angle of the front of the inlet may not be right for that though.
Area 2 looks like the reflection of the opposite rudder, complete with black stripe. Angle might be too shallow for that though. Could be something external to the aircraft altogether.
The distinct line pointed to by 3 is the reflection of the top of the engine cowling. The 2 different shades are likely the transition in surface materials. The 2 shades don’t match the color of the 2 materials, but may show the difference in ambient light reflected off them. Could also be the dark section is the shadow from the opposite tail projecting directly onto the APU intake’s surface. Option 3 is that the back of that reflection is lighter because of the reflection of bright light off the left tail onto the engine.
4 is the reflection of some blue sky and 5 possibly some clouds.
In fact, the lighting/shadow conditions probably highlight the shapes. Besides, the visible reflections have blurry edges.
As with all shadows, when objects are closer to the surface their shadow is projected onto, their shadow is sharper. Same goes for reflections onto diffuse surfaces.
We’ll see, would confirm before transferring this directly to the gospel library.
Yeah, I say you’re right on the money, you can even ray trace which surface each of those shadows originates from (some are darker because they are just multiple shadows combined).
The only reason for faceting would be stealth (faceting isn’t optimal for aerodynamics) but:
a) that surface is in an unexposed area of an aircraft that is meant to fly high altitude, so no point
b) multiple inconsistently angled facets like that would actually be anti-stealth for specular reflection. Effective VLO shaping is all about REDUCING the number of angles where rays are reflected. “Faceted” doesn’t simply equate to “stealthy”, there’s science to consider as well.
c) it would provide absolutely no benefit for front aspect stealth compared to the smoothly swept back surface shown in other photos, not even for surface waves…. in fact it may even increase forward scatter due to the multiple surface discontinuities pointing in random directions.
d) there’s bigger fish to fry than the fronts of those intakes
Yes, my background can be applied to this topic. I have worked for a well known European defense giant on ground sensors. My job was not related to R&D rather than to benchmark testing for various applications.. Most notably on future soldier programmes.
So what you’re saying is you have as much insight into classified detection ranges of aircraft IR detection systems as a …. computer operator (computers are on aircraft too you know?)
Noticed your input is at a very high level, not a lot of detail goin on there 🙂
*sigh* next wannabe please….
How on earth are you managing to evaluate the RCS average figures? All you have is a base figure from a frontal aspect and know way in hell of guessing the rest, not to a reasonable degreee of accuracy anyway. Sorry but your figures are worthless.
Its called guessing. No science or fact involved whatsoever. I believe some obscure voodoo method of coming up with RCS was used too, something strange like counting surfaces :rolleyes:
I’ve never heard anyone call three “several” before now
While everyone’s being pedantic, 3 is actually the very first number that qualifies as being called “several”. Several: More than 2, less than many.