I didn't realize I was GF.. it was in response AFB's response about the possible sale of Su-35s. to China.
ah, gotcha.
I didn't realize I was GF.. it was in response AFB's response about the possible sale of Su-35s. to China.
Aircraft carriers are not a priority for China. J-20 has plenty of combat radius, especially when couple with aerial refuelers. Varyag is for study only, not for operation. Once fusion power is a reality in a few decades, fusion powered fighter planes would have unlimited combat radius.![]()
I still think this points to a strike/aircraft not a fighter something with a range as good if not greater then the SU-34 because the JH-7 isn't excatly going to change the balance its not even as capable as a tornado.
And the Air data probe on the nose.
Looks like the second J-20, b/n 2002 are out and doing taxi trials.
Key Publishing Ltd Aviation Forums - View Single Post - J-20 Thread 7
At current time, i could not find any direct link..
Anyway, some small external changes.
The MLG doors have been altered.
And the Air data probe on the nose.
Well its official, the second J-20 prototype, 2002 has flown at the Chendu factory field, Dieno has some interesting comments, and other posters on our sister forum Sino Defense have noted that 2001 has been flown to another airfield. Both aircraft had been sitting at Chengdu together for a week or so. Whether you're a fan or no the J-20 is a significant accomplishment, I have an idea that 2001 will get to the real flight testing away from the limelight, but she has been very succesfull in the public portion of her roll-out. There has been an officiall first flight ceremony with lots of tour buses etc for 2002, so hopefully the wall climbers will continue the unauthorized Chegdu daily airshow coverage for 2002.
Oh and for you Sweetman fans, this airplane has been out there and whether or not they have radar or this or that, there really is little doubt that they are prototypes, and the lack of changes in 2002 indicate that they are fairly confident of their overall design. Its public debut indicates that this is a flagship, and I believe that they will make every attempt to field this aircraft ASAP, but in what quantities and with what capabilities? It is an important statement and a great PR success for the PLAAF. Cheers Brat
Just a follow on question to Air Force Brat. Your statement relative to the "overall design", were you alluding to the outside final configuration of the aircraft? Maybe I don't quite understand what you meant by that statement? IMHO, overall design means everything that is included with the aircraft. Just needs your clarification, thanks.
Oh and for you Sweetman fans, this airplane has been out there and whether or not they have radar or this or that, there really is little doubt that they are prototypes, and the lack of changes in 2002 indicate that they are fairly confident of their overall design. Its public debut indicates that this is a flagship, and I believe that they will make every attempt to field this aircraft ASAP, but in what quantities and with what capabilities? It is an important statement and a great PR success for the PLAAF. Cheers Brat
all it means, and I have said this elsewhere, is that the lack of external change means that they are comfortable with the final external config
that has nothing to do with internal changes - anyone who thinks that the internal fitouts etc are gold knows bugger all about aircraft or platform engineering.
this is not a gold article no matter what the enthusiasts might argue. I suspect that the chinese, just like JSF have done systems development off platform on other aircraft (like catbird), to speed it up.
Not sure if anyones posted this video yet
最新æ*¼20 (J20): Latest Combat Maneuver Tests on 2012.03.20 - YouTube
There's one thing i must ask about this video, the sequence at 0:30, when the pilots moving the flaps etc, on the horizontal stabilisers there appears to be 2 independant flaps.
Is that normal for a 21st century aircraft? May seem a silly question to ask, but i can't think of any other i've seen which operates like that, and then, why do it? What aerodynamic properties would that bring to the table?
An outstanding observation Rob and something that lots of folks miss, those are more properly referred to as flaperons, which are inboard, the next control surface on each side outboard are elavons. Their function is the key to their name, as while they are flaps, and ailerons in the traditional sense, they also perform the pitch function of elevators. This is somewhat archaic tech as the aft mounted deltas of the Convairs, 102 and 106 had flaperons and elevons. In addition as you have noted the J-20 has distant coupled canards, which also perform the pitch funtion and in fact may be the primary pitch control in landing and takeoff. You have in fact hit on the Flight Control System, which is quite an engineering achievement in and of itself, and in fact is the key to the J-20s overall manueverability. The aft mounted delta main wing has made this neccesary in order to have full roll and pitch control and as Haavarla has noted, the all flying verts are canted outward and also aid in the pitch control. Cheers Brat
https://medium.com/war-is-boring/chinas-building-stealth-fighters-faster-and-faster-665e6e41db0f
6th J-20 prototype has flown, number 2015 apparently only shows minor differences from the earlier more radically different prototype 2011 with a housing for an IR sensor, more LO orientated outlets and supposedly a new coating.
The only real difference for this prototype is slightly different tail surfaces. After all, 6 prototypes in you'd think the final design is becoming more set in stone.
The article ends saying the WS-15 engine is still in development.