• 제목/요약/키워드: Test Institute

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RF COMPATIBILITY TEST BETWEEN KOMPSAT AND TTC STATION

  • Ahn, Sang-Il;Choi, Hae-Jin
    • Journal of Astronomy and Space Sciences
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    • 제16권2호
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    • pp.191-198
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    • 1999
  • Results of RF compatibility test between KOMPSAT(Korea Multi-Purpose SATellite) and TTC(Tracking, Telemetry, and Command) station are described. S/C(Spacecreft) RF Test, telemetry test, command test, ranging test, and tracking receiver test were performed with respect to pass/fail criteria. To provide physical RF interface between KOMPSAT and TTC equipment, direct low cable and antenna-to-antenna interface were implemented. Through RF compatibility test, it was fully demonstrated that KOMPSAT and TTC equipment are functionally workable.

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KC-100 전기체 정적 구조시험 (KC-100 Full-scale Airframe Static Test)

  • 심재열;정근완;이한용;이상근;황귀철;안석민
    • 한국항공우주학회지
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    • 제42권1호
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    • pp.67-75
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    • 2014
  • 항우연에서는 복합재 소형항공기(KC-100)에 대하여 15가지 전기체 시험조건과 7개의 국부적 시험조건들에 대한 전기체 정적구조시험을 수행하였다. 시험요구도, 시험일정, 시험체 및 더미구조, 시험하중산출, 시험장치, 시험장비 등을 소개하였다. 수십개의 제어채널을 사용하는 전기체 구조시험의 하중제어의 정확도를 살펴보기 위하여 U1의 시험데이터를 분석하였다. 분석결과 각 채널별 데이터 획득된 하중값은 허용오차인 SNPE(Static null pacing error)값 이내에서 잘 유지하고 있음을 보였고 본 논문의 저자가 제안한 시험의 하중제어오차 크기 정의방법을 적용한 결과 U1 시험의 하중제어 오차값이 8.6N 이었고 나머지 전기체 시험조건들에 대한 시험데이터를 분석한 결과도 보였다. 마지막으로 U1시험에서 자세제어장치에서 측정된 반력들이 시험하중 증가와 함께 변하는 것을 보였고 전기체 구조시험에서 반력변화 발생의 요인들에 대하여 기술하였다.

Contribution of thermal-hydraulic validation tests to the standard design approval of SMART

  • Park, Hyun-Sik;Kwon, Tae-Soon;Moon, Sang-Ki;Cho, Seok;Euh, Dong-Jin;Yi, Sung-Jae
    • Nuclear Engineering and Technology
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    • 제49권7호
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    • pp.1537-1546
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    • 2017
  • Many thermal-hydraulic tests have been conducted at the Korea Atomic Energy Research Institute for verification of the SMART (System-integrated Modular Advanced ReacTor) design, the standard design approval of which was issued by the Korean regulatory body. In this paper, the contributions of these tests to the standard design approval of SMART are discussed. First, an integral effect test facility named VISTA-ITL (Experimental Verification by Integral Simulation of Transients and Accidents-Integral Test Loop) has been utilized to assess the TASS/SMR-S (Transient and Set-point Simulation/Small and Medium) safety analysis code and confirm its conservatism, to support standard design approval, and to construct a database for the SMART design optimization. In addition, many separate effect tests have been performed. The reactor internal flow test has been conducted using the SCOP (SMART COre flow distribution and Pressure drop test) facility to evaluate the reactor internal flow and pressure distributions. An ECC (Emergency Core Coolant) performance test has been carried out using the SWAT (SMART ECC Water Asymmetric Two-phase choking test) facility to evaluate the safety injection performance and to validate the thermal-hydraulic model used in the safety analysis code. The Freon CHF (Critical Heat Flux) test has been performed using the FTHEL (Freon Thermal Hydraulic Experimental Loop) facility to construct a database from the $5{\times}5$ rod bundle Freon CHF tests and to evaluate the DNBR (Departure from Nucleate Boiling Ratio) model in the safety analysis and core design codes. These test results were used for standard design approval of SMART to verify its design bases, design tools, and analysis methodology.

수송류 항공기용 금속계 제동패드의 다이나모시험 절차 (Dynamometer Test Procedure of Metal Brake Pad for Part 25 Aircraft)

  • 김민지;김경일;김경택
    • 한국항행학회논문지
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    • 제27권6호
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    • pp.821-827
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    • 2023
  • 본 연구에서는 국내 및 미국의 항공기 기술기준과 기술표준품 표준서를 분석하여 수송류 항공기용 금속계 제동패드의 비행시험 인증을 위한 합치성 증명 시 요구되는 다이나모시험절차를 도출하였다. 제동장치의 설계개조는 중대한 변경으로 분류되어 부가형식증명 및 부품등제작증명이 동시에 요구된다. 다이나모시험 항목은 미국의 제동장치 기술표준품 표준서인 TSO-C135a 규정에 따라 비행시험의 적합성을 판단하는 기준으로 비행시험 시 요구되는 주요 시험항목 중 설계착륙-정지 시험, 가속-정지 시험 및 최대 하중상태의 착륙-정지 시험을 선정하였다. 다이나모시험 조건은 항공기 제조사가 제공하는 주요 사양에 따라 정해지며, 제동패드의 조건, 감속도 및 시험횟수 등은 TSO-C135a 규정에 따라 정의하였다.

Determination of Cyclogram for Liquid-Propellant Rocket Engine

  • Ha, Seong-Up;Kwon, Oh-Sung;Lee, Jung-Ho;Kim, Byoung-Hun;Kang, Sun-Il;Han, Sang-Yeop;Cho, In-Hyun;Lee, Dae-Sung
    • International Journal of Aeronautical and Space Sciences
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    • 제3권2호
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    • pp.59-66
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    • 2002
  • A vertical test stand based on launcher propulsion system was constructed and several tests for the determination of cyclogram were carried out. To make an accurate estimation, static and dynamic pressures were measured and analyzed. Especially, static pressure measurements using fast response sensors without extension tubes were used to determine operation sequence more evidently. The standard operation times of final valves were determined in cold flow tests with an engine head, and fire formation time in combustion chamber was checked in an ignition test with an ignitor only. On the basis of these tests, ignition sequence was established and combustion test cyclogram was finally determined. According to combustion test, test results were well matched with the determined cyclogram within 0.05 sec.

탄약 간 정밀교전을 위한 시험평가기법 연구 (A Study on the Test and Evaluation Methodology for the Precise Encountering Scenario between Ammunitions)

  • 하종수;박영식;이한진;김용재;곽윤;박민규
    • 한국군사과학기술학회지
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    • 제21권6호
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    • pp.776-783
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    • 2018
  • This paper proposes an improved test and evaluation methodology to be conducted for a in-flight threat-countermeasure encounter scenario. Although the conventional test method adopted in the precedent researches allows high precision and safety, such full-scale method is practically not appropriate to apply to small-scale test rounds for evaluating the subparts of the ammunition. To address this problem, this study suggests a readily-applicable, small-scale test and evaluation method of the subpart of the ammunition in firing test. In the threat-countermeasure encounter scenario, the results of several tests demonstrate that the proposed technique does not deteriorate the precision when the engagement point should be adjusted.

한국형발사체 7톤 파워팩 시스템 고주파 신호 분석 (The Analysis of High Frequency Signal for 7tonf-class Power Pack System of KSLV-II)

  • 소윤석;이승재;이광진;김승한;한영민
    • 한국추진공학회지
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    • 제20권3호
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    • pp.96-102
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    • 2016
  • 7톤 엔진 시험 전에 엔진 시동/정격구동/종료 특성을 확인하고자 나로우주센터 터보펌프 실매질 시험설비에서 파워팩 시험을 수행하였다. 가스발생기 연소실의 동압은 0.2 bar이하로 측정되어 연소 불안정을 발생하지 않았고, 터보펌프에 장착된 RPM 및 가속도 센서 신호 분석 결과, 예측 RPM 범위 안에서 파워팩 시험이 안정하게 수행되었다는 것을 확인하였다.

폴리머 현수애자의 신뢰성 평가 및 복합가속열화 방법 (Reliability Evaluation Criteria and Multi-Stress Aging Test for Polymer Insulator)

  • 박효열;강동필;안명상
    • 한국전기전자재료학회:학술대회논문집
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    • 한국전기전자재료학회 2004년도 하계학술대회 논문집 Vol.5 No.1
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    • pp.469-472
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    • 2004
  • There have been numerous accelerated aging laboratory tests for evaluating suitability of polymeric materials and devices. Aging test for materials and its full scale device has been conducted, but poor correlation of aging test such as service experience were observed. Service experience plays a key role in the utility section of composite insulators. A meaningful and reliable accelerated aging test is needed for evaluating composite insulator. During the service these insulators are subjected to aging stress such as humidity, pollution, and electrical field, and erosion and tracking of the weathershed occurs. This paper presents the criteria of reliability evaluation and evaluation facilities for 22.9 kV suspension composite insulator. We adopt the criteria of reliability evaluation consist of two test methods. One is CEA tracking wheel test for examining the tracking and erosion performance of composite insulator. The other is multi-stress aging test for examining effects of environmental factors such as UV, temperature, humidity, etc on composite insulator.

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PV모듈의 I-V특성 시험을 위한 Solar Simulator의 측정불확도 요인 분석 (Analysis of Solar Simulator's Uncertainty Factor for Photovoltaic Module's I-V curve test)

  • 강기환;박지홍;김경수;유권종;안형근;한득영
    • 한국전기전자재료학회:학술대회논문집
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    • 한국전기전자재료학회 2006년도 하계학술대회 논문집 Vol.7
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    • pp.5-7
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    • 2006
  • In this paper, we analyzed the elements of measurement uncertainty on electrical performance test which are the most important things in photovoltaic module performance test. Repeating the performance test by 6 men, the measurement uncertainty could be calculated. In this experiment, Solar Simulator (A-Class pulse type) used for domestic certificate test of PV module is Pasan IIIb (Balval, Switzerland). The possible elements of the measurement uncertain that could effect electrical performance test of PV module are reference cell, spectrum correction, error from measurement repetition, test condition, stability and uniformity of artificial solar simulator. To find the measurement uncertainty, 6 men repeated the test by 10 times. And the results were that numerical average value was 124.44W and measurement uncertainty was $124.44W{\pm}0.75W$ with 95% confidence level for 125W PV module.

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대구지역 개의 심장사상충 감염실태 (A survey on the infection rate of Dirofilaria immitis of dogs in Daegu area)

  • 임현숙;조유정;서동균;송동준;이춘식;배영찬
    • 한국동물위생학회지
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    • 제26권2호
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    • pp.129-134
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    • 2003
  • A survey of canine heartworm(Dirofilaria immitis) infections among dogs in Daefu area was performed from February 2000 to October 2002 using a microfilarial test and an antigen test(AGEN$^{TM}$ Canine heartworm). The infection rate of 220 dogs(96 males, 124 females) was 23.2%(51/22) by the microfilarial test, but was 23.6%(52/220) by the antigen test, revealing that 1 of 52 antigen-positive dogs were microfilaria-negative in the peripheral blood. All dogs that were microgilaria-positive were also antigen-positive. The infection rates of heartworm in dogs at the age of < 1, 1-3, 4-6, 7-11 and 12-15 years were 2.7%, 17.4%, 41.0%, 42.9% and 57.1%, respectively. Based on the fact that the antigen test is more accurate than the microfilaria test. The infection rates of heartworm in dogs by housing of indoor and outdoor were 6.9% and 46.4%, respectively. Based on the fact that outdoor housing is more infectious than indoor housing.