• Journal of the Korea Society for Simulation
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• v.21 no.4
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• pp.25-33
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• 2012

Armed helicopter is an integral part of armed forces, which conducts vital missions, such as anti-armor attack, close air support, escorting air assault operations, and reconnaissance. A typical cockpit arrangement of armed helicopters has been a tandem configuration. This is to reduce the frontal area, which in turn increases the forward speed as well as reduces the chance of being hit by enemy fires. However, many armed helicopters in the world are now being developed as a side-by-side configuration. Such configuration is quite different from the conventional cockpit arrangement in light of the crew communications and situational awareness. Therefore, the main objective of this study is to find the optimized combination of mission tasks among pilots in a side-by-side configuration cockpit by measuring the workload using the NASA Task Load Index method. The experimental results indicate that the workload of crew members differ as disparate tasks are being performed.

• Defense and Technology
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• no.3 s.265
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• pp.10-19
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• 2001

• Defense and Technology
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• no.8 s.150
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• pp.48-59
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• 1991

소련 지상군은 현재 총 4천5백여대의 헬기를 여러가지 목적으로 운용하고 있다. 무장헬기가 2천50대를 차지하고 있음 주력은 1천4백20대의 Mi-24로 구성되어 있다. 물자, 병력 수송용으로는 1천여대의 Mi-8외에 Mi-6, Mi-26, Mi-10 등을 운용하고 있으며, 별도로 전자전 장비를 갖춘 2백여대의 Mi-8를 운용하고 있다. 소련 헬기로서 최초로 실용화 되어 양산된 Mi-2도 6백여대 이상이 아직 일반 목적용으로 운용 중에 있다

• Journal of the Korea Academia-Industrial cooperation Society
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• v.21 no.8
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• pp.147-153
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• 2020

Developments in aircraft require safety verification through flight testing for many hours with prototype design and production. The test evaluation step of performing flight tests was an important process that determines the success in the development of the system. In particular, safety development through flight tests in the armed flight test is important for the development of attack helicopters. In the development of attack helicopters, the evaluation period and cost related to the armed flight test are closely related to the required ammunition requirement. Therefore, this paper presents the amount of ammunition required for the military flight test between attack helicopter developments through an analysis of the AH-1 helicopter in a similar case and ADS-44-HDBK of military specification. The AH-1 can be used to calculate the ammunition demand by considering the exclusion of redundant firing tests and configuration differences. In the case of the machine gun-equipped configuration, approximately 10,500R was required, and approximately 324R was required in the case of a rocket-mounted configuration. In addition, if the armed integrated bench is used properly, it is expected to promote efficiently the flight test in the armed flight by identifying the possible risk factors with armed flight tests and excluding them.

• Defense and Technology
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• no.8 s.198
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• pp.46-57
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• 1995

• Defense and Technology
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• no.7 s.125
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• pp.66-71
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• 1989

헬기는 수용할수 없는 추가적인 비용의 소모와 공중역학상 적용하기 어려운 중량의 증가없이는 속도와 기동성 및 무장수준의 한계에 도달하였다. 헬기가 비록 지표면 비행기술로 200mph의 속도로 비행할수 있다해도, 10배 또는 그 이상의 속도로 비행하는 열추적 다탄두 전술미사일의 표적이 되는 것이 어느 시점인가를 물어야될 것이다

• The Journal of Korean Institute of Communications and Information Sciences
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• v.39C no.11
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• pp.1088-1093
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• 2014

The structure of the fire control system(FCS) of a light armed helicopter and effective logistics support was taken into account in the proposed common weapon interface module(CWIM) for a distributed FCS. The pros and cons of a distributed FCS and a centralized FCS were analyzed, then a CWIM which can be applied to the weapon interface module of a distributed FCS was designed and fabricated. Integration tests between the proposed CWIM and a weapon simulator were conducted to ascertain whether or not the proposed CWIM could be applicable to a distributed FCS. We expect that the CWIM design approach method secured through this study will be helpful in mitigating cable work of the FCS which will be applied to a Light Armed Helicopter and controlling various weapons.

• Defense and Technology
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• no.8 s.294
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• pp.64-71
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• 2003

Rooivalk에 채택된 항전장착물은 프랑스의 Sextant가 주 개발자이며 3개의 다기능 디스플레이를 갖는 NVG 호환 G-Cockpit도 포함된다. Thales는 Topowl HMSD도 공급하는데 이것은 Denel사 Cumulus 공장에서 개발된 센서 터렛과 Pilkington Optronics와 공동개발한 Noctua PNVS와 연계된다. Rooivalk의 TDATS는 Topowl과 함께 작동하는 Cumulus사 Argos-780 EO 센서 터렛을 사용하고 있고 열상장비, TV카메라, 레이저 거리측정기, 레이저 표식기 그리고 자동추적기로 구성되어 있다.

• Journal of the Korea Institute of Military Science and Technology
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• v.17 no.6
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• pp.786-792
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• 2014

In this paper, we propose a novel method which can be applied to test and verify the stabilization-tracking performance of Gun/Turret Driving System(GTDS) for Light Armed Helicopter(LAH). In real system, GTDS is connected to TADS/SMC and drived to aim at the target with 20mm gun. But each equipment is separately developed during exploratory development stage, so GTDS cannot be tested under real system state. We suggest new configuration of test system for evaluating the stabilization-tacking performance, in which TADS and SMC are replaced by vision acquisition unit and processing unit, respectively.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.41 no.9
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• pp.726-733
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• 2013

The rotor blade of helicopter is the core component determining helicopter performance and requiring low noise and low vibration because the blade becomes the major source of noise during flight. The performance analysis of candidates rotor blades is very critical because LCH(Light Civil Helicopter) will be developed parallel with LAH(Light Armed Helicopter) as an international upgrade program based on the existing platform of foreign civil helicopter. This research was aimed to recognize the performance of the candidates rotor blades compared with the newly developed foreign rotor blades and to investigate the feasibility about developing korea unique shape rotor blades by analysis the rotor performance and noise. The result of this research can be used for the target performance index during negotiation with foreign helicopter company and developing korea unique shape rotor blades.