Glad you like it, what do you think about the rear? too Flankerish?
The way the exhausts are designed, rear aspect IR and RCS signatures will doubled or even tripled from front. Not good. Dead meat for the Raptor.
Exhaust nozzle convergent coupled with throttle setting control thrust. Everything on a body create its own RCS signature and contribute to the overall RCS value of the body. The convergent-divergent mechanisms of an afterburning turbojet engine are no exceptions, if anything, they are the major RCS creators of the rear aspect.
Take a look at 'iris' style exhaust convergent-divergent nozzle above. It is called 'iris' because the mechanisms works the same way the human eye controls its pupil opening. Look at all the 'feathers' and the gaps between them. Those are corner reflectors and I have explained plenty enough here on how dangerous corner reflectors are to designs intending to be radar LO.
Now look at the F-22 exhaust convergent-divergent mechanisms above. They are simpler in designs and because there are less mechanical 'doodads' such as actuators and 'feathers' the F-22 exhausts are far less RCS contributors than exhausts with the 'iris' convergent-divergent exhausts.
The downside to the F-22's exhaust mechanisms is that it restrict thrust vectoring to 2D, whereas with the 'iris' style, the exhaust TV can be 3D, provided there are sufficient clearance between nozzles, which lead us to the controversial subject of design philosophy, specifically engine placements. Wide area engine placements have advantages and disadvantages. Personally, I have never been a proponent of wide area engine placements. The argument here is that for any reason, from bird ingestion to battle damage to 'Acts of God', in the event of a catastrophic engine failure that result in an engine explosion, the other engine would be somewhat protected. Given the fact that the airframe area between the engines are not empty but contain fuel, wirings and assorted mechanical items, an exploding engine will create enough collateral damage to render the aircraft unflyable anyway.
In the event of a non-exploding engine failure, widely spaced engines will create asymmetric thrust that can send the aircraft into a flat spin, which can be nonrecoverable. The combination here is speed, altitude, attitude and how far apart are the engines that the resulting asymmetric thrust will send the aircraft into a flat spin. An extreme example of asymmetric thrust is the C-17A Engine-Out Compensation System (EOCS) software upgrade to the aircraft's FLCS during take-offs and landings. For EOCS, the critical engine is the most outboard one on each wing if its companion outboard engine on the other wing fail. The software upgrade, upon sensing engine failure, would command a rudder deflection to compensate for the inevitable yaw (lateral) movement by the aircraft.
AOPA Online: AOPA Pilot's "An Invitation to Fly" - Beyond the Private
If one engine fails, for example, asymmetric thrust can cause the airplane to yaw severely. Much of the multiengine flight training curriculum centers on handling such emergency situations.
Fighter aircrafts with multiple engines do not have as wide engine placements as multi-engined transports, nevertheless, asymmetric thrust is still a potential problem for pilot training. The F-14 and F-15 have wider engine placement schemes than the F-18. The wider the engine placements the higher of some energy loss when there is thrust. Any mechanical engineer will tell you that it is better to have thrust as much inline with the main longitudinal axis of the body as possible. It is necessary that thrust be in parallel, but the closer to the central axis, the greater the concentration of their combined thrust to the longitudinal axis, the more energy efficient the TV system. The downside is that the closer the engines are together, there will so little room for movement that 2D vectoring is the only option.
3D vectoring require more complex flight control laws --
IF -- the desire is to automate the thrust vectoring. Automation require the removal of some of the decision making process from the pilot, which is
NOT always a positive. The US have done extensive testing on the integration of propulsion into flight control laws, of which the C-17A EOCS is one deployed example, here is the history...
Propulsion Control of Airplanes
In July 1989, the tail engine of the DC-10 of United Airlines Flight 232, enroute from Denver to Minneapolis, sustained a "catastrophic uncontained failure" that created a hail of shrapnel, slicing the hydraulics lines of all three independent systems, leaving the aircraft "marginally controllable" at 37,000 feet. Contrary to the realistically motivated consensus at that time that this flight should have ended in disaster, Captain Al Haynes, with the help of United Captain and DC-10 Flight Instructor Dennis Fitch, quickly improvised a way to keep control of the aircraft by maneuvering the throttles of the remaining wing engines. To the great amazement of aviation officials, the crew managed to bring the aircraft to a crash landing in Sioux City, Iowa, saving the lifes of most of those on board.
NASA - NASA Dryden Fact Sheet - Propulsion Controlled Aircraft
Propulsion Controlled Aircraft is a computer-assisted engine control system that enables a pilot to land a plane safely when its normal control surfaces such as elevators, rudders, and ailerons are disabled. If used on commercial aircraft, PCA and follow on projects could help reduce the number of aircraft accidents.
Essentially...If we have engine failures, there is still a good chance of recovery and survival via flight control surfaces, aka 'dead stick' landing as UA 232 demonstrated...
Deadstick landing - Wikipedia, the free encyclopedia
A deadstick landing, also called a dead-stick landing or forced landing, occurs when an aircraft loses all of its propulsive power and is forced to land. The term is a misnomer, as the flight controls in the majority of aircraft are either fully or partially functional, even with no engine power. So it is not the "stick" (flight control actuator) that is "dead", but rather the engine(s). The term refers to the wooden propeller (the "stick") being stopped in an engine-out setting. The fixed position prop actually creates less drag and increases glide speed.
But what if the aircraft loses some of its flight control surfaces, that is where PCA enabled flight control laws can help. Thrust vectoring works on similar principles as PCA but it is about the incorporation of
DELIBERATE off-axis thrust not to recover a damaged aircraft but to radically enhanced its flight regimes. So asymmetric thrust can be exploited to good ends.
The PAK-FA's wide engine placements allows 3D vectoring, however, we do not know the extent of TV automation. Is the pilot allowed individual nozzle vector controls? Now that would remove a lot of mathematical complexity from the flight control laws but would transfer the burden to the pilot. After all, what good in having a feature if you do not know how or allowed to use that feature? Remember UA 232 above where the pilot had to manipulate the throttles himself. This mystery alone begs us to wonder how does Sukhoi view the pilot. Is he a 'killer' first and 'flyer' second? Or would the TV training and operation be so intensive that he would be so busy working the nozzles that he can lose situational awareness and lose the fight?
3D vectoring is best when there is so little aerodynamic forces to exploit that in order to change aircraft attitude, an alternate force is required, this would be at very low airspeed, so low that even if there is any advantage to be gained over the F-22, the F-22 would have to be either battle damaged or at so low an altitude that the F-22 pilot has next to no room to maneuver. The Soviets/Russians do not have a good history of avionics and ergonomics. We knew that even before the Soviet Union collapsed.
Do not be gullible and impressed by that airshow 'cobra' maneuver. It was done with extraordinary airmanship acquired through years of flight experience and natural abilities. That is not how we want our air forces. We want an efficient combination of high flying capabilities and human instincts now. The American philosophy is -- make the aircraft do the flying as much as possible so the pilot can be a 'killer' primary and 'flyer' secondary. When the aircraft exceed maneuvering requirements just through aerodynamic exploitations alone, TV capability is gravy and having 2D only allow some pilot control and some automation without overly complex flight control laws. This is like creating one hundred above average airborne killers in one year instead of ten excellent ones in two years.
Raptors are extinct.
Raptor happens to be vegetarian. Poor thing!!
Raptor is a classification of bird...
Bird of prey - Wikipedia, the free encyclopedia
Birds of prey are birds that hunt for food primarily on the wing, using their keen senses, especially vision. They are defined as any bird that hunts other animals. Their talons and beaks tend to be relatively large, powerful and adapted for tearing and/or piercing flesh.
Dead meat for the Raptor, baby...