Unless the tank is in a mountainous region 600 meters above http://members.home.nl/7seas/radcalc.htm the radar horizon can be possible
Radar horizon isn’t the problem, power, cooling, aperture are the problem, and even if it is possible why do you or anyone think it is a good idea to give an active hardkill protection on a battle tank a long range radar?. This is the case of proparganda go way over the top.
I am just quoting their statements. I was even going to mention a tank with an attached drone called pterodactyl.
Be skeptical,be critical of what you read. Don’t just blindly believe something because it fit your agenda.
http://www.lektire.me/prepricano/djordje-anicic-smena_945
P-18 wasn’t part of battery but it was part of division (somewhere you can find P-12 instead P-18 because P-18 was added to another division, so that isn’t clear), it tracked targets from +50km, but P-15 start tracking target from at least 23km (detailed info from book). Then they start tracking it with SNR-125, that is how procedure goes.
I just looked at the link you gave, can’t find “P-18 tracked target from +50km ” anywhere, and they didn’t specified the type of radar either.
Only the search radar (could be P-15 or P-18 or P-12) detect the aircraft from 23 km.
Then when the search radar indicate that the plane was at 14-15 km away, Dani ordered his crew to use SNR-125 fire control radar and illuminate the direction for target, they find it after the third search, so the aircraft must have gotten even closer.
BTW F-117 isn’t 0.001m2 it was during early pole measurement (compete with XST) but that was with early RAM (or maybe without RAM at all?), but RAM was improved trough service so RCS is very likely smaller probable lot smaller maybe 0.0001m2? So S-125 target and guidance radar couldn’t detect it from mentioned distance if it was same conditions as pole measurement but it wasn’t. So using best possible RCS numbers isn’t that useful. And modern SAM network (with fast datalinks) make things much harder even for VLO that is why Israel doesn’t want Syria to get S-300 even though Israel is getting F-35.
USAF said F-35 is stealthier than F-117, at that time they claimed F-35 estimated RCS to be 0.0015m2, so there is little reason to believe that F-117 RCS goes below 0.001 m2. I haven’t heard anything about F-117 changing RAM either. If i understand what they wrote correctly, according to the book, SNR-125 didn’t detect F-117 from distance >15 km, no clear information on whether P-12/18 or P-15 was used to detect F-117 at 23 km.SAM nowaday are much better than what they were in Serbia war, however modern VLO aircraft are not the same as F-117 either, they have RWR, Jammer, DIRCM, IRST, Radar and weapon with longer reach.
http://www.ausairpower.net/APA-S-125-Neva.html
P-15 is part of S-125 system. P-18 isn’t. P-15 is target acquisition radar. So no way P-18 could be used to down F-117 and I don’t see why folks constant mentioning VHF radars. They don’t guide missiles, they could only guide fighters on VLO targets. This is very important for Russia or China but for weaker countries it isn’t.
If you look at your source, they said P-12/18 are optional for S-125 battery
[ATTACH=CONFIG]261978[/ATTACH]
VHF radar are not used to guild missiles because their beam width are wide, which result in big miss distance at long range. This is less of an issue at close range.
SNR-125 is missile guidance radar(X-band radar), SNR-125 locked F-117 for more then 15km, info about that is book written by member of SAM crew which was there when F-117 was downed.
I haven’t seen the book you mentioned so it would be helpful if you can give us the screenshot of the paragraph, with that being said they also claimed that they shot down a B-2 (totally nonsense btw), so i would take everything they claimed with a grain of salt.
anyway, since you like to use AusAirPower, according to them, the detection distance of SNR-125 is:
[ATTACH=CONFIG]261979[/ATTACH]
SNR-125 can detect target with RCS = 10m2 from 80 nm (148 km), according to radar equation, 10 times reduction in RCS will decrease detection range down to 56%, so a target with RCS = 0.001 m2 will be detected at 7.87 nm (or 14.5 km) so not so far from the claimed value of 15 km. Can be explained by variation in aspect.
This is common myth. Radar which first detect was P-15 and then with second radar which guide missiles (SNR-125). This is what SAM crew members confirm couple times and this is logical if you check how S-125 works
All sources I can find about the incident said they used the P-18 to detect/track the F-117, I have seen the interview but I don’t think they mentioned the system used is P-15. So if you have some contrary evidence please show.
The estimated range of detection of a helicopter or aircraft, the radar means of a tank “Armata”, 20 – 25 km. This power allows you to intercept cannon shells at a range of up to 50 meters
That make absolutely no sense. If radar cross section of a cannon shell is 0.001 m2 and it is detected by ARMATA’s radar from 50 meters away, by radar equation we know the same radar will detect an aircraft with RCS= 10 m2 from 508 meters away, you just can’t get the “100 km” value and we haven’t touch the cooling, aperture and clutter issues. Logically, why anyone want their hard kill APS radar to have long range?
BTW you can believe in 100km AESA radar on ARMATA…. So you are capable believe in anything
Confirmatory bias and extreme nationalism is a bad combination
the 2nd source was from General hostage stating F-35 stealthier, the 1st source if I remember correctly the airforce stating both 5th gens previously before being golf ball and steel marble. Shania explained that the F-35 had a change in material, but a drastic 500 times decrease in size is hard to believe. I believe ActionJackson stated the F-35 was now the size of a Pea about a year ago from a thread saying .00001m2 if I recall correctly.
500 times is 25dB different.
Aspect and frequency are important, if you looks at the picture earlier, rcs at offbore spike is18 dBsm while frontal rcs is – 18dBsm. Total variation of 36 dB which is about 4000 times. For frequency, frontal rcs at 0.1 Ghz is 0 dBsm, at 1 Ghz is – 18dBsm, and rcs will down even further at 8 Ghz and higher.
is that off of lockheed and if it is should my trust be that easy to give like the sudden RCS change on both 5th gen aircrafts?
It didn’t came from lockheed Martin
-18dBsm without RAM, but yet it was tracked with S-125 from +20km (SNR-125 radar), one crew member even mentioned +50km, he was operator of P-15 radar in tv interview. I wouldn’t mentioned what Zoltan said becuase his statements aren’t back up by other members of battery (he said they tracked F-117 while it was still in Bosnia).
Pay attention, RCS is – 18dBsm in frontal arcs between 0.4-2Ghz. F-117 was tracked by P-18 which operate in VHF aka 30-300 Mhz.
Some of us don’t even bother taking any of Lockheed RCS claims that seriously. Some gave values of .005 and .0001m2 and now they all believe the F-35 is now 500 times smaller than the F-22. I do not even care anymore if I hear .000001m2 for their 6th gen(even though they stated that stealth has to be sacrificed). No one is entirely that convinced yet
Or only you, anechoic chamber measurement shows that F-117 metal model have RCS of -18 dBsm between 0.4-2Ghz. Now go up in frequency and add RAM.
LMFS: the thing is, anti-stealth radar tends to be L-band or lower
Radar need to operate at lower frequency to be effective against stealth
F-117 model without RAM:
[ATTACH=CONFIG]261936[/ATTACH]
The MiG-25, likewise, was a 20k ton empty-weight fighter that could achieve Mach 3 with engines producing only 100 kN of thrust each
Engine thrust isn’t a fixed value, it changes with speed and altitude, mig-25 has very high V-max because it’s engine and inlet provide high thrust even at high speed and altitude. Similarly the Bell X-1A with straight wingcan reach Mach 2.44 because rocket engine doesn’t lose thrust with speed.:max_bytes(150000):strip_icc()/bell-x-1-large-56a61c545f9b58b7d0dff7a2.jpg)
A stealthiness augmentor composed of curved vanes ejectors is not exactly the same thing as a radar blocker
Again,
Pratt points out that the F119 and F135 are the only production engines with stealthy augmentors. Their design eliminates conventional spray bars and flame holders and integrates multi-zone reheat fuel injection into curved vanes that block the line-of-sight to the turbine.
New to this forum …
Assuming you forgot that there is a third dimension, which is not visible in this diagram…
One would would assume the Russians are not so naive in engineering, remember my university lecturer in Australia who was Russian and very impressed with his ability
Hi, KGB
Noone apart some forumers speculatin said it is a radar blocker… Did they?
No
Screech, the F135 and the JSF Engine War
Posted by Graham Warwick at 3/17/2011 1:33 PM CDT
For those of us who thought screech was the noise made by GE/Rolls and Pratt & Whitney in their war of words over the JSF second engine, here’s the background to comments made this week about screech problems with the F-35’s F135 engine.Testifying before the House Armed Services Committee on Tuesday, JSF program executive officer Adm David Venlet said afterburner screech on the F135, which prevents the engine from sustaining full thrust, “caused us to avoid certain portions of the flight envelope.” Instead, F-35s have flown to other points in the envelope to keep flight-test going. Kits are being installed to overcome the problem, he said.
So what is screech and what’s the fix?
Pratt says screech is a phenomenon caused by pressure pulsations in the afterburner at low altitude and high speed. The problem was discovered during development testing around March 2009, having previously been encountered – and solved – in the F-22’s F119 engine, from which the F135 is derived.
Pratt points out that the F119 and F135 are the only production engines with stealthy augmentors. Their design eliminates conventional spray bars and flame holders and integrates multi-zone reheat fuel injection into curved vanes that block the line-of-sight to the turbine.
Building on its experience with the F119, the fix for the F135 includes “minor hardware changes to the fuel system, reduced aerodynamic leakages and upgraded software,” says Pratt, adding that the modified engine “now provides full max augmented thrust throughout the flight envelope.”
A kit has been developed for flight-test engines, and two have been modified. The production configuration will be validated this year in both the CTOL/CV and STOVL variants of the F135, Pratt says.
I have asked GE/Rolls whether their F136 has a screech-free stealthy augmentor. Watch this space for their answer.
And here it is:
GE/Rolls says the F136 has “no known” screech problem, but acknowledges it is four years behind Pratt in development. An augmented F136 was demonstrated recently to the JPO on its Evendale test stand without experiencing screech, but the engine has not flown yet.
GE/Rolls also points out that afterburner screech was a problem of fighters long before stealth came along
8 AAM when they finally fit the extra AIM-120 on outer bay door. There are various hints of that configuration
The F-35 program office is looking at adding capacity for another AIM-120 AMRAAM radar-guided air-to-air missile in each of the jet’s two weapons bays, increasing internal—and thus stealthy—missile loadout by 50 percent, program director Lt. Gen. Christopher Bogdan said March 22. Speaking with reporters after his speech at a McAleese/Credit Suisse conference in Washington, D.C., Bogdan said, “There is potential … to add a third missile on each side.” The upgrade would likely be part of the Block IV program of F-35 enhancements, but “that’s something I know the services and all the partners” are interested in. Bogdan said this would not require some special version of AMRAAM, but “the same AMRAAM missiles that we carry today, just an extra one; probably on the weapons bay door.”