The simple fact is that the Israeli’s have always been outnumbered yet they always prevail because of poor training and little skill on the Arab side of the equation.
Israeli armed forces r very well trained…no doubt about it. But one has to read a non-biased history/analysis of 1973 war in order to realise wot really happenend during that war.
No one can really complain about US helping Israel cos on the other side soviets also equiped arabs to the teeth.
It seems to me that surprise played a massive role in these wars. I mean look at the fighter losses ratios for 1967, 1973 and 1982. Israel achieved almost total air superiorit in 1967 while in 1973 they were forced to cease all airforce ops for at least 16 hours. Egypt/syria gained a lot in 1973 through their surprise tactic, and if it wasnt for the incompetent political/military high command (when egyptians stopped their assualt after achieving their objective in spite of the fact that syrians were asking them to continue to keep israeli forces occupied…which in turn gave israelis a chance to regroup and deal with them one by one) result may have been somewhat different.
Finally, no doubt that Syria lost a large number of aircrafts in 1982 (probably 82-92). OTOH, israeli claims of no loss r without a doubt dumb…though the overall ratio must have been heavily in israeli favour.
Early model Mig-29s were dynamically unstable designs with hydraulic control. Yet their agility is time proven.
AFM published an article on Mig-23 in Oct 2003 issue, according to which Syria is currently operating around 60 floggers of which 40 r highly modified to MLD standard. Russian ML/MLD upgrade pace seems to have increased in the light of 1982 syrian/Israeli air war. As for 1982 conflict, according to Air Enthusiast (July/Aug 2002 issue), syrian floggers played only a secondary role with 10 losses (4 M models and 6 MF models) while their pilots claimed 5 kills (none of which can b confirmed).
A few months back, there were indications that the negotiations for M2K-5 were at a rather advanced stage and some were even implying that the deal will b finalised soon. In the light of this, its rather strange that IAF sent in an evaluation team for SMT. :confused: But, perhaps there is an alternative explanation and the two may not b linked??? IAF mayb interested in upgrading their existing Mig-29 fleet to SMT standards, since it’d b somewhat illogical/expenisve to maintain 2 almost different a/c, i.e. Mig-29 for IAF and Mig-29K for IN. That said, purchase of 125 M2K-5 with TOT (and im sure IAF will also upgrade their existing fleet) wont b cheap by any means in comaprison with Mig-29SMT (without taking into account the operational costs). Unless im mistaken india has to delay the discussions for scorpenes for at least a year due to lack of funds and currently they have a large number of projects going which r consuming a lot of funds.
PS. I have to admit that sometime back i used to think IAF is only showing interest in M2K-5 to derail PAF’s efforts to aquire the fighter. however, I was rather surprised to learn recently that PAF is still very much interested in M2K-9 :confused:
Too much patriotism perhaps?
But there also many who can and do look beyond the veil.
The flyaway cost of a Mirage 2000-5 is about 30 to 35 million estimated, probably the most 40 million (possibly 30 to 40 mil for a Block 52 F-16 now flyaway cost). As a rough rule, flyaway cost tend to be 50% to 60% of the contract price.
True.
In addition, the avionics may be somewhere around 25-45% of the fly away price.
PS. Unless im mistaken, UAE is paying around $80 mil per unit for its F-16E/F…but this includes everything from A-Z almost.
Cost of labour does come into this equation, but there r various other factors dat also influence the fly away unit price. A very simplified example is dat if 500 ppl r working on a single line that rolls out 2 aircrafts per month (in france and china), the overall costs of labour and raw materials will b much cheaper in china, which would obviously influence the unit price making it considerably cheaper in china. OTOH, the quality of an aircraft is also a major determinant. Once again an example is the J-7II which probably costs around $2-3 mil, while the cost of F-7MF is expected to b around $7-8 mil in spite of the fact that there wont b much difference between their empty weights.
The actual interview also talks of 2 mission computers.
Usman shabir (of Pakdef) clarified the issue…the aircraft has a full FBW with a redundant hydraulic system. According to him, the next issue of AFM will have a 5-page special on JF-17…may clarify more issues.
Turkey’s cancellation of these projects seems to stem from their recent financial hardships as well as political issues within EU…they need some strong backing from Germany/France, and linking of their future projects with EU companies is likely to pay off handsomely.
guys does the Mirages of PA, which went through ROSE upgrades..capable of firing BVR?? any more info on that upgrade (radar range etc would be welcomed)
This is a million dollar question…and it seems that PAF doesnt want anyone to know about it, hence a lot of conflicting reports from them (firing of a BVR AAM from an upgraded platform, i.e. mirage, appeared in newspapers last year, while reports about T-darter have also surfaced). Even Janes seems to b confused about this issue. :confused:
An educated guess would be that if they dont have this ability they soon will aquire it (depending on how long they remain in service). Rose Mirages’ Grifo M has enough range for BVR missiles and if one of Darter series BVR is not employed already, then chinese FD-60 (which janes recently linked with F-16) may b used as an alternative or even SD-10.
As we already saw in the numbers above, the operating envelope of the FC-1 already gives good TWR when it is needed. By the time you need high maneuverability for a WVR dogfight, you’ve most likely have fired off your bvraams and have used up a portion of your fuel. At that point, the FC-1 would be flying at or over unity.
Good point and it raises another question.
Under most scenarios (between most countries), the strike/escort formations r gonna b rather limited in numbers and most fighter pilots would probably get a single BVR shot b4 it becomes WVR. If so, would it b worth carrying a large combination BVR/WVR missiles; i.e. 4/4 or 6/6???
How much is 50% fuel for both?
About 1,150 Kg for both.
Why don’t they just go to Klimov and try for RD-33-10M, which at MAKS 2001 was reported to be approximately 103kN (10.5 tonnes thrust).
After 2010, Klimov is expected to have the VK-10M (which the RD-33-10M is a prototype for), which will be 108-113kN.
Flight International, 24-30 June issue, 1998 did in fact link VKS-10 with FC-1. However, we havent seen any developments in this regard and it does seem that CAC opted for a safer option. One should also remember Klimov General Director Alexander Sarkisov did not exclude the possibility that an upgraded RD-33 with thrust-vectoring nozzle, dubbed the RD-133, could be offered to power combat aircraft, including MiG-29 tactical fighters, in several other countries. So as crobato put it…may be later.
TWR during a conflict will obviously b kept under close observation…depedning on the actual mission in question.
For Gripen, TWR with 50% fuel, 2 EM A2A missile, 2 IR A2A missile is 0.98, while with 100% fuel, 2 EM A2A missile, 2 IR A2A missile is 0.88.
http://home.iae.nl/users/wbergmns/info/jas39.htm
FC-1 comes mighty close.
Assuming an empty weight of 6400Kg (upper end), 2 Pl-9 (300 Kg including launching rails) and 2 SD-10 (460 Kg including rails), TWR with 50% fuel is 1 while with 100% fuel its 0.88.
bharat
The FC-1 uses the RD-93 engine, not even the RD-33K has such spc.
Now dats another confusing issue. :confused:
Whereas Aviation Week & Space Technology (see the link i provided in one of my posts above) describes RD-93 as an an in-depth modification of the MiG-29’s RD-33 turbofan, developed for an order from China, Janes describes it as a further upgrade of RD-33K (see the following link for Janes article). we can only guess about it fuel efficiency, MBTO etc. :rolleyes:
http://www.aeronautics.ru/archive/research_literature/aviation_articles/Janes/topics/plasma_stealth/Aircraft%20and%20Propulsion%20Systems.pdf
PS. Hope, crobato and GoldenDragon’s statements regarding ferry range would b sufficient.