I’m surprised with all of the modernizations to the main wing they didn’t opt to change the inlets to a series closer to the wing roots, something akin to the F-105. The nose of the aircraft was already cramped, and to change to side body-mounted inlets would of alleviated some of the space problems.
Trident is more of an all or nothing option. Use it and the world’s nuclear arsenals are all in. Don’t use it and preserve peace.
Smashing a Mach 6 target with a bucket of bolts is nonsense. SDI failed all but the most spoon fed of targets, so ineffective the tests required the integration of strong uniquely signatured homing transmitters in all downflight targets. Its not going to be very vulnerable at all.
I just don’t think it makes sense for more than a small quantity of bombers. The faster you burn a candle the faster the wax is all gone. It would be too expensive of program.
That clarifies it then. I was thinking he was saying it didn’t use fm to range with which is not true as far as I’m understanding it.
1. The SA-2 wasn’t successful, it wasn’t even a warhead fragment that hit the plane and the pilot didn’t even notice anything until he found it after landing.
I hardly consider the SA-2 a failure. The SA-3 was a pared down SA-2. The SA-3 took down a wobbly goblin. SA-2 took down, percentage-wise, as many U.S. aircraft per flight as enemy MiG’s in any war. Not per attempt, but per flight.
How does the Zaslon pick up ultra low flying targets without a pds mode? I’d think you’d need it against the clutter.
Four Mig-31s flying roughly 200km apart can scan up to a WIDTH of 1,000km, using a datalink.
They form a virtual radar with a scan width of 1,000km. And the datalink is digital.
The F-14D master can act as director for the steering of each slaved array. Otherwise, it is just overlaying a series of independent scans upon a master map. You want the master in control or you leave huge gaps in coverage.
I don’t quite understand what you were trying to say…but if you’re saying that MiG-31 should get squadron datalink, it has it for 25 years now.
But can one aircraft slave the scan modes of the others into a cohesive pattern or do they just link their displays? Big difference.
I’m not sure you want the Dornier Do 335 Pfeil as an example as it had a prop on the nose, too, not just in the tail.
There is no advantage to either installation. They both suffer induced drag penalties. The advantage of the pusher is the free space in the front end. Otherwise the propeller is going to create more drag in both positions than if it used a turbine. If one wants raw speed performance than nothing beats a turbine. Propellers offer simplicity in design and are easier on the budget.
I would dare to speculate the Su-27 program is the future of the air defense forces whereas the MiG-31 – even modernized further – has a shorter shelf life of perhaps ten more years at the most. The compatibility of these two systems to work together is probably more important than one system stealing the shine of another. (Since MiG is no longer producing the latter then all they can hope for is to bleed the existing program for future monies.) I wouldn’t put it past the program to develop a powerful datalink system together akin to the F-14D’s where four or more aircraft can chain their radars together to more than double their effective scaning scope.
BINGO! Too many ignorant people don’t realize this. They always point to the F-15s advantage in thrust, acceleration, etc. But the F-18E/F has the advantage in everything you said, and that makes all the difference in the world. Sensors, radar, avionics, cockpit design is all better in the Super Bug.
Your logic makes the F-16 Block 60 and beyond so much better than both.
btw – The latest F-15E aesa has every feature capability the F-18E has but it more powerful. The manufacturer just doesn’t include all of the functions in the stock software.
The four target limitation of Zaslon may be due to its coded pulses for which it illuminates a target. It might only have the ability to send four specifically coded illumination pulses at a time whereas the AWG-9 used coded data links separate from the single illuminator carrier signal. Don’t get me wrong, there are probably a near infinite number of coded sequences to send out the illumination signals, the fire control itself is perhaps limited to sustaining and managing the manipulation of the code for four unique patterns at a time. The targets for the AWG-9 are systematically hit with radiation from the same signal source for targeting updates, which becomes less effective in regards to timing granularity as the distance increases between missile and launching aircraft – hence the need for active terminal guidance. (Even at the speed of light it does take critical time for the signal to travel out to the target and return, plus the time to steer the signal from one point to the next.) The Zaslon can simultaneously mark four targets with separate signals if I’m understanding how it works. So technically speaking the Zaslon is the much more sophisticated of the two.
The outer layer of the tvc’s on the f-22 are insulated to minimize reflection of infrared wavelengths. The skin of the entire aircraft is also insulated, but in this case its like a cotton tee, where the underlayment is actively cooled, so that it doesn’t emit in the traditional wavelengths when under air friction. The B-2 was the pioneer of these technologies. The F-117 is usually credited with these techniques, but it only truly used passive techniques on the skin and relied on a combination of an inter-cooling system and physical louver screens for hiding the engine emmisions.
A Mirage III is able to physically dominate the MiG-21, too, but that doesn’t say much about the Mirage III or MiG-21 in general. They are just designed around disimilar flight envelopes.