I can’t get on the website (cnki) I might look for this on some sort of academic platform.
I’m on the website now, but issue is, I need the title of document rather than this which only has chapter title. I am looking for anything missile related now.
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Near identical. Still, good addition.
Yes. I guess PL-8B will have similar range or more range.
PLAAF and PLANAF aircraft not operated of PL-9 & PL-9C
PL-8B flare resistant higher PL-8.
But same AIM-9M & AAM-3 ?
Check this out, in game files of PL8B is actually insanely quick.
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R-27T if it was good
R-27T was built in the early 80s idk why it’s being compared to a 2000s missile
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So much bigger as well, but similar speed I guess is where the comparison comes from. Could be just a more manoeuvrable version with IRCCM. Might be quite nice actually considering the range.
The acceleration of the PL-8 to begin with was one of the bonus’s. Of course, all AIM-9L and other non-IRCCM missiles are already considerably underperforming in-game so the jump to IRCCM seems more noticeable than it should.
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It’s a joke about about the PL-8B being fast, not any sort of serious comparison
Find it, it’s 某空空导弹固体火箭发动机改进设计及试验研究
I searched its chapter headings and somehow it works, I don’t know how it can recognize scanned files.
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Nice, I was getting worried because I couldn’t find the posted document on the forums, I swear it was on here a while ago.
PL-8B is not in game, he made it with the information that we have online, Python4 is in game.
in files
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New missile?
Where is it, cnki?
Summary:
Spoiler
空军的主要任务之一是保持空中优势。在最近几年,由于新型的先进飞机、武器系统和战术的发展与运用,这个任务变得十分困难。因此,空军必须加倍努力对付各种可能发生的新的威胁,而改进机载空空导弹系统和使用先进的导弹是这个努力的重要环节。 某空空导弹是一种高机动性、全向攻击型战术导弹,也是我空军目前近距离格斗的主要武器之一。该产品是上世纪八十年代从国外技术引进的具有世界先进水平的第三代空空格斗式导弹,自国产化鉴定至今已生产了二十年,为了使我国空军适应当今空战,提高空军的作战能力以及提高该导弹的作战性能,总体单位对导弹控制舱作了改进,导引头由单元探测改进为四元探测,改进后的控制舱抗干扰能力大大提高,从而提高了探测精度,增大了迎头探测距离。这就要求该导弹系统具备足够的动力射程,否则就起不到射程远、命中精度高、威力大的作用。按照国外的经验,通常采取改进导弹外形或增大发动机装药的方式提高导弹动力射程。 本文对导弹固体火箭发动机进行了改进设计和试验研究。根据与总体单位和用户进行协调,确定对A导弹增程目标设定为1～2kmn。射程的增加依靠推力装置火箭发动机的改进来实现。通过对发动机总体结构、工作原理和推进剂性能分析,确定了以增加发动机装药量提高总冲的方案,完成了发动机结构设计、推进剂装药设计及内弹道计算,并根据空空导弹的使用要求与发射环境,进行了发动机地面环境试验、地面点火试验及靶场飞行试验研究。 增程改进后导弹固体火箭发动机的装药量增加了12.55kg,总冲增加了32.055KN·s,达到了导弹动力射程增加2km的预定目标
One of the Air Force’s primary missions is to maintain air superiority. In recent years, this task has become extremely difficult due to the development and use of new and advanced aircraft, weapons systems and tactics. Therefore, the Air Force must redouble its efforts to deal with various possible new threats, and improving airborne air-to-air missile systems and using advanced missiles is an important part of this effort. A certain air-to-air missile is a highly maneuverable, all-directional attack tactical missile, and is also one of the main weapons of our air force in close combat. This product is a world-advanced third-generation air-to-air combat missile introduced from foreign technology in the 1980s. It has been produced for 20 years since its localization and identification. In order to adapt our Air Force to today’s air combat and improve the Air Force’s combat capabilities capabilities and improve the combat performance of the missile, the overall unit has improved the missile control cabin. The seeker has been improved from unit detection to four-element detection. The improved control cabin’s anti-interference ability has been greatly improved, thereby improving detection accuracy and increasing The head-on detection distance is increased. This requires that the missile system has sufficient power range, otherwise it will not be able to achieve the functions of long range, high hit accuracy and high power. According to foreign experience, the missile’s power range is usually improved by improving the missile’s shape or increasing its engine charge. This paper conducts improved design and experimental research on the missile solid rocket motor. Based on coordination with the overall units and users, it was determined that the range extension target for the A missile was set to 1 to 2kmn. The increase in range is achieved by improvements in the thrust device rocket motor. By analyzing the overall structure, working principle and propellant performance of the engine, a plan was determined to increase the total impact by increasing the engine charge. The engine structure design, propellant charge design and internal ballistic calculation were completed, and based on the use of air-to-air missiles Requirements and launch environment, the engine ground environment test, ground ignition test and range flight test research were conducted. After the extended-range improvement, the charge of the missile’s solid rocket motor increased by 12.55kg, and the total impulse increased by 32.055KN·s, achieving the intended target of increasing the missile’s power range by 2km.
Can’t seem to download it though. Does fit the description of a 4 element seeker.
Right found it. The Modified Design and Experimental Study of the Solid Rocket Motor of the Missile - CNKI
Anyone registered on CNKI?
Saying controversial stuff like “new threat to B-21” is to garnish views. It’s just propaganda again, there currently does not exist a missile especially suited for engaging stealth aircraft and a hypersonic missile will not have any viable IR based seeker system.
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I’ve recently noticed photos of a new PL-12 batch mounted on J15. Anyone has anything on this?
Can’t confirm but could this be PL12A?
The text on the side of the missile looks new but this does not look like a service missile. This seems to just be a display model of some sort. There is no clear distinction between PL-12 and PL-12A at this time.
What we know is that, so far, all in-service live ordnance will have a visible target detection device of some sort whether it be laser or RF based. This missile is smooth and does not have the large rectangular windows seen on live PL-12 ordnance.