The velocity vector roll is one of those nice things the Typhoon does well, it can get so much controllable alpha as well as roll that after a handful of rotations it can bleed off so much energy its almost at a standstill midair, leaving the screaming EJ200’s to boost it back up to speed. Just as the airframe, those engines are very powerful for their size, their technology except for thrust vectoring (which is being tested at MTU) is broadly comparable to the F119 in the Raptor, few stages, blisk construction, high turbine inlet temperature, moderate pressure ratio, good fuel consumption for its bypass ratio of 0.4 to 1. It’s war setting gives it a dry thrust of more than 15500 lbs thrust without afterburner, over 21000 with afterburner. For its weight class those engines give an amazing acceleration to the Typhoon, and its wing loading is superb.
Think about it……dry thrust of an engine in the same weight class as the GE F404 and dry thrust almost matching the older engines max thrust. Yummy.
The Tornado was an adaption of a strike aircraft, had exceptional CAP range and endurance, a good interceptor, but not something you’d want to be in a turning fight.
Over G…..The thrust vectoring improves roll rate in the Raptor not because of differential action (they only operate together up or down) but because the TV nozzles take work out of the horizontal slabs in pitch leaving them do do more for roll control.
I’ve got that book, and his other book that has history of both turbine and piston engines.
The stated goal of the IHPTET program by phase III was to have demonstratable technology in jet engines that would double the effective performance of the “base level advanced turbofan” of the late 80’s, being the prototype engines for the ATF program, which became the Raptor. The F119 already has a generous specific thrust in terms of its airflow, but it is quite a heavy engine when coupled to its 2D vectoring nozzle. The goal was to double the thrust to weight of the baseline engine, so much of the technology isn’t in making a big heavy engine more powerful, its to take hopefully hundreds of pounts of weight out of the propulsion system, which has a huge impact on range, altitude, instantaneous and sustained turn rate, the less mass you have the better wing loading and specific excess power. The Air Force verion of the F-35 has a propulsion system weight of 6354 lbs, that’s a BIG engine and every pound of weight they can remove in future versions can only improve the thing. Same thing with the F119, the actual engine is slightly below its weight specification, but the nozzle despite having 3 generations of exerience with 2D vectoring nozzles, eg F-15 SMTD, YF-22 and finally EMD production model F/A-22 is above its weight specification. It is an effective but heavy technology and i don’t blame them for looking for other avenues in order to reduce weight.
One technology is called fluidic nozzles, simply speaking it uses bleed air from the engine to modify the engine exhaust profile such that there is effectively vectoring effect with next to no moving parts, greatly reducing weight and mechanical complexity. The computational fluid dynamics labs are working to understand the physics of the effect and are working under the aegis of IHPTET to bring it into fruition.
As for supercruise, i’ve seen many shots of in house weapons systems sims that Paul Metz flew, and while having quite a generous amount of fuel left and at 80 percent throttle was supercruising very quickly. A good program that has many unique shots including the CAD damage analysis model (amazing how little room there is for fuel inside that aircraft, it showed location and volumes of all fuel tanks, they’re tiny except for the one that sists behind the pilot leading aft to the intakes and the 2 saddle tanks that sit inside the tailbooms.) The program was on the Canadian Discovery channel and it was called Flightpath. If you can buy it do so, despite being dated somewhat by time the interviews are very clear specifically on supercruise performance and RCS limitations.
The official site has stated its capable of Mach 2 plus at high……in addition to supercruising up to Mach 1.72, typically between 35-40000 ft.
As for thrust vectoring effectiveness at high altitude, its very effective, do a little trig, the amount of thrust effectively perpendicular to the flight path when those nozzles move up 20 degrees is probably more than what the aero surfaces can push the nose around with.
You’re right there, typical cadmium plated tools would rot the fasteners right off once they got up to temperature, marking airframe pieces was equally difficult because common items like felt pens were corrosive, even a graphite pencil etched the titanium. They literally threw all tools into a vat which stripped off all cadmium and other coatings so they’d be safe.
Chlorine in city water also had an effect, welds failed that were done in summer but those done in wintertime, that were cooled with non chlorinated winter water held up fine. Fluorine for the same reason, the drinking water had trace amounts to fight tooth decay so they had to find sources which didn’t have that contamination.
I think the Foxbat leading edges were titanium, but that was about it.
True, there is no sound on that file. Not that one expected sound on an old archival film of flight testing.
Here’s a goodie, the video from the first flight of the A-12, the CIA single seat predecessor to the SR-71.
Somebody needs to get the pics and video of the super STOL Herc they planned to use for rescuing the American hostages in Iran over 20 years ago. The one video clip i saw of it of the first STOL test the lift rockets fired prematurely and it was a write off.
Originally i think there was to be 2 aircraft, the one that flew was only the aerodynamic demonstrator. It could be classed in the same league as the Rafale and Eurofighter for low observables, might take a few square m off the signature but not stealth as US companies are used to.
To make an analogy US Navy types used to see a radar return on a wake but not see the ship and mutter “Ah, there’s the Kirov”, it had some limited low observablility features on it, in the same way stealth aircraft CAN be detected by a combination of very low frequency radar which can see it coming generally, and a very high frequency radar which doesn’t detect the aircraft but rather the turbulence the airframe and engines produce, similar to how doppler radar can detect tornados. The SR-71 Blackbird i’m told when it lit the afterburners, the plume, the enormous energy it put into the air and I’m not talking IR, but just the pure mass airflow velocity delta, it was very detectable by radar.
I disagree, if you read a little history German fighter production was never higher than at the end of the war. The problem is there was no fuel for them. The fuel manufacturing facilities were far easier to knock out then an aviation manufacturing process that had almost become a cottage industry. Very small individual shops making small parts that were delivered to various subassembly places and them those parts in turn were sent to delocalized final assembly facilities. Modular contruction is not a new concept, Having no other way to keep production up the Germans were forced into decentralization of all manufacturing. Just as the British were to a lesser extent. They just moved a lot of theirs out of range of the Luftwaffe bombers, which never did develop a bomber in the B-17 class, never mind B-29. Most bomber development was keyed to direct army support by Hitlers whim, didn’t help that that the head of the German air force was a morphine addict who didn’t know how to let his field commanders give input into what was really needed. So didn’t need the long range aircraft. Lucky for us.
Active cancellation was talked about during a 60 Minutes clip a decade ago, it has it.
Known about it for over a month, go to media relations and video gallery, some good footage in there.