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ASRAAM and AMRAAM for JF17 ??

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have come by with an undiscussed brochure of JF17 in which AMRAAM (BVR) and ASRAAM (WVR) were written as main weapon

JF-17 specifications (Ideas 2014)2.jpg


JF-17 specifications (Ideas 2014)2.jpg

ob_5db7e3_sraam-infographic.jpg
 
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have come by with an undiscussed brochure of JF17 in which AMRAAM (BVR) and ASRAAM (WVR) were written as main weapon

View attachment 269985

That's just them taking the liberty of using weapons names as general class of weapons, i.e., asraam is a reference to advance wvr missile, AMRAAM to SD-10 and JDAM to Chinese sat guided bombs.
 
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That's just them taking the liberty of using weapons names as general class of weapons, i.e., asraam is a reference to advance war missile, AMRAAM to SD-10 and JDAM to Chinese sat guided bombs.
No reference can't be written as

they could have easily written as SD10 A and PL5IIE (or bvr and wvr missile)
 
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No reference can't be written as

they could have easily written as SD10 A and PL5IIE (or bvr and wvr missile)

If you look closely, they are referring to weapon class, anti ship missile instead of C-802, anti runway instead of durandal and so forth. It would have been slightly intriguing if it had just mentioned ASRAAM but AMRAAM and JDAM gave it away.
 
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A couple thoughts ...

AMRAAM is an abbreviation for " Advanced Medium-Range Air-to-Air Missile"
ASRAAM is an abbreviation for "Advanced Short Range Air-to-Air Missile"

While commonly used for Aim-120 and Aim-132 respectively ... however in this case ... I think they have been used in terms of their abbreviation (for SD-10 & PL-5 IIE) not the specific weapon systems they commonly represent ...
 
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View attachment 269987

Guys, tell me about this system on tail of Thunder above the engine!

JF-17 Thunder’s Threat warning system, tail housing & drogue chute

The chaffs are used against radar-guided threats, i.e. Surface to Air Missiles (SAM) or interceptor aircraft whereas the flares are for infrared threat and heat seeking missiles such as enemy aircraft or Man-portable air-defense systems (MANPADS). In JF-17, the Chaff/flare dispensers are located under the ventral fins. Around 100 chaffs/flares can be carried at one time. The chaff/flare load out depends upon mission planning (mainly mission type/formation/load out etc). Using 5-10 chaffs/flares in one bundle will increase their usage to up to 10 times.



Chaff/flare dispensers are visible just after the air brakes and before the engine exhaust. Inside the cockpit the threat management system is located in the left auxiliary panel which directly manages its usage.





The JF-17s delivered to PAF till 2008 had no chaff/flare dispensers installed in them. Seen in above photos a specially marked JF-17 (Sr.# 07-101) flying during 23rd March parade 2007 with no chaffs/flares installed and an operational No.16 Sqn JF-17 at Dubai Air show 2011 with visible signs of chaffs/flares box installation.

Tail housing of JF-17 Thunder:

The top of the tail housing contains Missile air warning sensors (MAWS), a navigational light, Ultra High Frequency (UHF) communication antenna and two electrostatic energy dispensers. MAWS are a part of self-defense electronic countermeasure system of the aircraft and work in collaboration with other sensors present in the frontal section of nose. The navigational light blinks repeatedly during landing and takeoffs.




Two electrostatic energy dispensers are visible on to top and rear bottom position of tail housing. They are used to disperse unwanted electricity to the air, which can cause problem in communication and navigation. A total of four similar electricity dischargers are also present on flaperons and horizontal stabilizers. These electricity dischargers deflect any lightning strike, making aircraft invulnerable to such extreme weather situations.



Present under the squadron emblem is the flight control & communication antenna, used to record flight control information from rudder, horizontal stabilizers and VHF/UHF communication.

Drogue chute section:



The rear tail section contains a drogue chute section, Radar Warning Receiver (RWR) and tail navigational light. Inset photo; the outward curved portion with a circular center houses the RWR system. The drogue chute section contains a breaking parachute used to decrease aircraft airspeed during landing. A landing without use of drogue chute is also possible, but it will require minimum amount of thrust, low airspeed, timely braking and equally good handling techniques.



The bottom portion of the drogue chute section contains a door lock, which is used to add/remove drogue chute in it. Necessary air crew related warning messages are also written on it.



A JF-17 moments after deploying drogue chute. Note the opened drogue chute section with hollow space.



Another close up of the empty drogue chute section with opened drogue chute door. The drogue chute is automatically disconnected from the aircraft and drops on the runway. An “all time standby” drogue chute collector team picks it up soon before any other aircraft lands at the runway.
 
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Well the integration and store simulations for these missiles have been performed since anytime the airforce can decide to buy and use this missile and also important for marketing since other airforce may want to use these missiles
 
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I doubt they are going to arm Thunder with any of the sophisticated US munition.Instead PAF might be going for Chinese/western/South American weapons of same category. MAR-1 is one such example.And who knows we might see new weaponry with AESA radar as it would bring in inherent ease of using more sophisticated weapons.
 
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The mentioned range is 1800KM. is it a combat range(go 1800 KM far attack and come back) or Ferry range(Just on way range of 1800) ?
 
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Americans would never give the ICDs required to integrate these systems
 
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