Author of the newsletter 'Sheldon's Military'๐Ÿ‡ฐ๐Ÿ‡ท. In-depth technical analysis of Korean defense technology.

Joined May 2022
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patreon.com/posts/next-generโ€ฆ Korean Next-Generation Fighter Testbed development program is gradually taking shape to replace the ROK Air Force's F-16 series fighters. This post has been uploaded as Free access.
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patreon.com/posts/inlex-koreโ€ฆ Hanwha Aerospace is developing intelligent 40mm unmanned air defense system (UADS) through rapid demonstration program ('24.12~'27.06). At this InLEX Korea 2026, vehicle-mounted 40mm UADS integrated with K239 Chunmoo chassis platform was unveiled.
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patreon.com/posts/kaav-ii-2-โ€ฆ KAAV-II Powertrain - part 2. Waterjet system & Power Transfer Module (PTM).
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patreon.com/posts/kaav-ii-1-โ€ฆ KAAV-II Powertrain - part 1 This article compiles information regarding engine, transmission, and integrated cooling system of KAAV-II powertrain. While fundamentally similar to EFV, platform features enhanced operability and incorporates CVT (HMT). Exploratory development prototype utilized MT883 Ka-524 engine, but system development phase will integrate modified DV27K-based engine.
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patreon.com/posts/mobile-sysโ€ฆ Next-gen Mobile Integrated Communication System (TICN-II) is being developed as multi-layer integrated communication network that integrates ground, airborne, and satellite links, aiming to achieve mobility and lightweight design by consolidating all communication equipment into vehicle.
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Sony A7C2 -> A7CR
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patreon.com/posts/2026-jointโ€ฆ 2026 Joint Firepower Exercise - 2 This post has been uploaded as Free access.
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patreon.com/posts/2026-jointโ€ฆ 2026 Joint Firepower Exercise - 1
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๊ถ๊ธˆํ•ดํ•˜์‹œ๋Š” ๋ถ„๋“ค์ด ๋งŽ๋˜๋ฐ, ํ˜„์žฌ KAAV-II ์‹œ์ œ์ฐจ๋Ÿ‰ ํฌํƒ‘์€ ์™„์„ฑ๋œ ๊ฒŒ ์•„๋‹ˆ๊ณ , ํฌํƒ‘ ๋‚ด/์™ธ๋ถ€์˜ ์ฃผ์š” ์ง€์ ์—์„œ ์‚ฌ๊ฒฉ ์‹œ ๋ฐœ์ƒํ•˜๋Š” ์ถฉ๊ฒฉ๋Ÿ‰์„ ๊ณ„์ธกํ•˜๊ธฐ ์œ„ํ•ด ์ œ์ž‘๋œ ๊ฒƒ์ž…๋‹ˆ๋‹ค. ๋”ฐ๋ผ์„œ ๊ตฌ์„ฑํ’ˆ๋“ค์€ ๋ชฉ์—…์ด๊ณ  ์‹ค์ œ ์ž‘๋™ํ•˜์ง„ ์•Š์Šต๋‹ˆ๋‹ค. ๋ ˆ์ด๋‹ค์˜ ๊ฒฝ์šฐ์—๋Š” ์•„์ด์–ธํ”ผ์ŠคํŠธ APS์˜ aCHR ๋ ˆ์ด๋‹ค๋กœ ๋ชฉ์—…์„ ์ œ์ž‘ํ•œ ๊ฒƒ์œผ๋กœ ์ถ”์ •๋˜๊ณ , ์‹ค์ œ๋กœ๋Š” ADEX 2025์— ์ „์‹œ๋œ ํ•œํ™”์‹œ์Šคํ…œ์˜ APS๊ฐ€ ํ†ตํ•ฉ๋  ๊ฐ€๋Šฅ์„ฑ์ด ํฝ๋‹ˆ๋‹ค.
patreon.com/posts/analysis-oโ€ฆ KAAV-II Specifications โ–ถ Length 9m, Width 3.6m, Height 3.2m โ€‹โ–ถ Combat weight: 35 tons (ยฑ10%) โ€‹โ–ถ Engine: MT883 Ka-524 (Prototype) / DV27K base custom engine (System Development) โ€‹โ–ถ Armament: 40mm CTA cannon, 7.62mm machine gun โ–ถ โ€‹Ammunition: APFSDS-T, TP, MPHE โ€‹โ–ถ Front armor 30mm APDS protection (over 1km), Side/Rear armor 14.5x11.4mm API protection (over 1km), Top armor 155mm HE protection (over 15m) โ–ถโ€‹ 3 Crew 20~21 Passengers โ€‹โ–ถ Maximum speed: 20km/h (Water), 70km/h (Road) โ–ถ โ€‹Unit cost: Approximately KRW 12 billion
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patreon.com/posts/analysis-oโ€ฆ KAAV-II Specifications โ–ถ Length 9m, Width 3.6m, Height 3.2m โ€‹โ–ถ Combat weight: 35 tons (ยฑ10%) โ€‹โ–ถ Engine: MT883 Ka-524 (Prototype) / DV27K base custom engine (System Development) โ€‹โ–ถ Armament: 40mm CTA cannon, 7.62mm machine gun โ–ถ โ€‹Ammunition: APFSDS-T, TP, MPHE โ€‹โ–ถ Front armor 30mm APDS protection (over 1km), Side/Rear armor 14.5x11.4mm API protection (over 1km), Top armor 155mm HE protection (over 15m) โ–ถโ€‹ 3 Crew 20~21 Passengers โ€‹โ–ถ Maximum speed: 20km/h (Water), 70km/h (Road) โ–ถ โ€‹Unit cost: Approximately KRW 12 billion
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patreon.com/posts/analysis-oโ€ฆ I've uploaded an "Analysis of KAAV-II Prototype Vehicle" to Patreon. KAAV-II exploratory development ('18.10~'25.06) program focused on developing marine propulsion technology, body transformation technology for marine operation, variable suspension system technology, and lightweight armor technology, as well as materializing operational concepts and analyzing/setting optimal military required performance through land maneuver prototype, marine maneuver prototype, and vehicle operability confirmation tests. System development program is scheduled to commence in 2027 and continue until 2032.
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patreon.com/posts/yonsei-aerโ€ฆ KTP1400 is turboprop engine to be mounted on MQ-105K MUAV Block-II. It was developed through "Medium-Altitude Performance-Improved Turboprop Engine Technology ('21.07-'25.08)" project, and plans to acquire Initial Flight Release (IFR) through "Propeller-Driven Aero-Engine Prototype Development and Engine Certification Demonstration Technology ('24.12-'28.12)" project. Max-continuous power achieved 1,400 hp, which is about 17% improvement over PT6A-67A (1,200hp). Also, HAF4500 turbofan engine is under development utilizing KTP1400 core engine through "Development of Core Technology for 4,500lbf-Class High-Bypass Turbofan Engine for Electrified Aircraft ('26.04~'29.12)" project. HAF4500 is 4,500lbf, high-bypass turbofan engine (BPR 4 ). It features application of Inter-Shaft Rotor and integration of ISG capable of generating 100kWe. โ–ถ Engine length 1,405mm, width 686mm, height 830mm. โ–ถ 2-stage Centrifugal compressor, Reverse-flow Annular combustor, 2-stage Gas generator turbine, 2-stage Power turbine, 2-stage Reduction gear โ–ถ Air mass flow 3.3kg/s, OPR 14:1 (Take-off 12.6:1 / Max. 19:1) โ–ถ SFC : 0.46 lb/shp/hr โ–ถ Max. rotational speed : Gas generator (Ng) 38,000 rpm, Power turbine (Np) 23,000 rpm
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patreon.com/posts/kf-21-fighโ€ฆ Compared to estimated figures, it was confirmed that mass production program cost rose significantly due to exchange rate and supply chain issues, etc. Including auxiliary equipment, CSP, M/F, facility construction, etc., unit acquisition cost for KF-21 Block-I fighter increased by 5.74% from initial projection. In 80-unit subsequent program, acquisition cost per Block-II fighter grew by approximately 10% over Block-I.
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patreon.com/posts/2026-sase-โ€ฆ Conference part 3 summarizes 35-ton Reusable Methane Engine being develop by Hyundai Rotem, Anti-drone UAV (V-5) under development by Hanwha Aerospace with ADD, and business status of Solid propellant additives of Dongin Chemical. Hyundai Rotem's 35-ton Engine is ORSC cycle Methane engine, targeting length 1.98m, diameter 1.3m, and weight 470kg.
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patreon.com/posts/2026-sase-โ€ฆ "Long-Range Air-to-Air Missile (2026~2033)" is system development program led by Agency for Defense Development (ADD) to develop LRAAM missile. While similar to Meteor in shape, this missile utilizes Ku-Band AESA seeker to enhance Detection range, Resolution, and ECCM capabilities, while improving tracking against high-speed, high-maneuverability aerial targets via Rapid beam steering. To support this, ADD is conducting "Air-to-Air Missile Integration Design Technology for Aircraft Integration ('24.12~'27.05)" project to evaluate optimized, lightweight architecture and verify core technologies in advance.
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In addition, this content covers projects related to ducted ramjet technology that were presented at the conference. Presentations included an air-breathing guided rocket, a high-speed launch test vehicle for demonstrating ducted ramjet propulsion technology, and a supersonic cruise target vehicle similar to the GQM-163 Coyote.
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