Ok, it was based on *one* of the missiles intended for the S-400 SAM 🙂
I love my little Canon A40 digital camera. It takes some pretty fabulous pics for a little cheap camera.
Nope, it was designed for long range AWACS intercepts and the like, and was based on the S-400 SAM.
It was recognised that it might require external target designation to the host aircraft to get such ranges.
a pic:
Well, I don’t think it went anywhere- I believe the R-37 was preferred. Is the S-400 SAM still in development?
Developer: Novator
Length: 7.4m
Diameter: 510mm
Weight: 750kg
Height of target: 3m-30000m
Warhead: HE frag (directional effect)
Warhead weight: 50kg
Guidance: active radar + inertial
Range: up to 400km
nah, I just think its a cool design.
Heres the only other pic of it I’ve seen:
Just wanted to share this pic I found, thought to be a Mikoyan test model for 1.42 and/or 7.01 programmes.
Who let all the idiots in?
Large sections of the diagrams are identical, even where the J-10 and Lavi differ. Look at the airbrakes for example- the J-10’s are mounted higher and are somewhat different, while the airbrakes in the drawing are identical to the Lavi’s. If you overlay the two pictures in photoshop, you can find lots of areas of identical or near identical drawing.
Do you really believe all the internal structures are identical to the Lavi? Come on now, show some sense…
Well a new wider angle (but conventional) HUD with UFC has been shown at MAKS, but we are talking about a cheap and easy upgrade here.
The Brazillian site seems to say that “H-4” is T-Darter.
T-Darter is ramjet powered, in the class of the Meteor rather than the AIM-120. It uses the A-Darter IIR seeker.
It all depends what you want to do.
If you want to fly at Mach 0.8 at 36,000 ft, then you want a high bypass ratio turbofan. Its the most fuel efficient at these speeds.
Ask Airbus or Boeing!
If you want sustained supersonic flight, a low – or no- bypass ratio engine is more fuel efficient. What happened in the 70s was everyone decided that we could cruise around subsonically and then use the afterburners if we needed some speed.
The reason why all the new gen engines are low bypass ratio – they are all designed for better supersonic performance. Improved technology allows higher temps, which gives better fuel efficiency.
A higher bypass turbofan will always be more fuel efficient at subsonic cruising however, but then we are talking fighters not cargo planes.
GE tried with the F120 to make a variable cycle engine which could vary its bypass ratio, but the added complexity was judged to make it riskier than the F119.
Ok people-
U Darter
Guidance: Two-colour infra-red
Weight: 96 kg
Range: 0.4 km – 10 km
The SAAF’s current short/medium range air-to-air missile, the U-Darter (Upgraded Darter) has been developed from the V3C Darter for use by the Cheetah. Changes include increased weight, warhead, speeds, a digital autopilot and an improved guidance seeker within the same dimensions of the Darter. The guidance unit consists of a dual-band cooled indium-antimonide IR seeker. Manoeuvrability is greater than 50g features three acquisition modes; cage, autoscan and helmet/radar designation. Service entry was during 1997.
R-Darter
Length: 3.62m
Weight: 118 kg
Diameter: 16 cm
Range: 50km (at high altitude vs closing high altitude target)
V4 R-Darter (Radar Darter) medium-range air-to-air missile is an all-aspect beyond visual range (BVR) air-to-air radar guided missile and is currently the primary medium range armament of the SAAF’s Cheetah C fighters and will also be integrated onto the new Gripen fighter aircraft being acquired for the SAAF.
The V4 is designed to provide immunity against electronic counter-measures and has an upgrade capability to meet any future change in the threat. The active radar seeker head, in conjunction with the modern radar onboard the aircraft, lets the pilot track multiple targets and launch more than one missile. It is capable of two modes: lock on before or after launch. In the lock-on before launch for short-range engagements, the seeker can be slaved to the aircraft’s radar or the pilot’s helmet mounted cueing system. The seeker is activated before launch and guides the missile all the way to the target .In lock-on after launch mode, for long-range engagements, the missile employs inertial guidance immediately after launch until the seeker is activated and homes in on the target.
It is based on Israel’s Derby AAM. Development of Derby began in the early 1980’s, with South Africa joining the development program and providing funding a few years later. The two projects parted later, and have some minor differences.
It entered service formally in 2001, though some sources suggest 1995.
A-Darter
Guidance: Two colour IIR (90 degree off boresight capable)
Weight: 89 kg
Length: 2.98m
Diameter: 166mm
Span: 488mm
Range: > 15km
* Uses TVC + tail controls
* Can lock on after launch
* advanced IRCCM techniques
* Will continue to fly towards target under autopilot if lock is lost
S-Darter
* Long ramjet powered range AAM project
* initial inertial guidance stage
* 30km range with ground launch, up to 100km air launched at high altitude.
* 20kg warhead
* Mach 2-3
* IIR seeker for terminal stage
* TVC + tail controls
T-Darter
* As S-Darter but with datalink.
So H-2 is R-Darter and H-4 is T-Darter.
Interesting 😉
Well, I’ve got a load more pics/plans of various T-4MS configs if you want. I posted the one closest the the T-60 sketches.
hey andi did you scan these images yourself?
I’d like to give you a few pointers regarding scanning methods if so….
Nice pics tho 🙂