• Title/Summary/Keyword: space qualification

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Research on Development and Performance Evaluation for Thruster of Reaction Control System for KSLV-I (KSLV-I RCS 추력기 개발 및 수행 평가에 대한 연구)

  • Jeon, Sang-Woon;Jung, Seul
    • Journal of the Institute of Electronics Engineers of Korea SC
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    • v.47 no.3
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    • pp.19-27
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    • 2010
  • KSLV(Korea Space Launch Vehicle)-I is designed as a launch vehicle to enter a 100 kg-class satellite to the LEO(Low-Earth Orbit). Attitude angles of the upper-stage, including roll, pitch and yaw are controlled by cold gas thruster system using nitrogen gas. The thruster for the KSLV-I is the main pneumatic valve in the RCS(Reaction Control System). In this paper, the design, function tests, and environment tests of the thruster for KSLV-I are described. The developed thrusters are experimentally evaluated and successfully passed the required qualification and acceptance tests.

Experimental Assessment of PBGA Packaging Reliability under Strong Random Vibrations (강력한 임의진동 하에서 PBGA 패키지의 실험적 신뢰성 검증)

  • Kim, Yeong K.;Hwang, Dosoon
    • Journal of the Microelectronics and Packaging Society
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    • v.20 no.3
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    • pp.59-62
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    • 2013
  • Experimental analyses on the solder joint reliability of plastic ball grid array under harsh random vibration were presented. The chips were assembled on the daisy chained circuit boards for the test samples preparation, half of which were processed for underfill to investigate the underfill effects on the solder failures. Acceptance and qualification levels were applied for the solder failure tests, and the overall controlled RMS of the power spectrum densities of the steps were 22.7 Grms and 32.1 Grms, respectively. It was found that the samples survived without any solder failure during the tests, demonstrating the robustness of the packaging structure for potential avionics and space applications.

Legalization of Tree Doctor System and the Role of KSPP (나무의사 제도 법제화에 따른 식물병리학회의 역할)

  • Cha, Byeongjin
    • Research in Plant Disease
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    • v.23 no.3
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    • pp.207-211
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    • 2017
  • In December of 2016, 'The Forest Protection Act' was amended partly in The National Assembly and the socalled 'Tree Doctor Act' was promulgated. Tree Doctor Act will be enforced from June 28, 2018. Under the new Act, none other than 'Tree Hospital' can do disease and pest management work for trees in public living space. The only exclusive qualification for tree hospital is a 'Tree Doctor', the government registered license which is newly established by the Act. To become a tree doctor, he/she must complete the tree doctor training courses in the designated 'Tree Doctor Academy' and pass the qualification test. Currently, Korea Forest Service is drafting the enforcement ordinances and regulations for the implement of Tree Doctor Act. When taking into consideration that the most fundamental and important discipline of the plant and tree health care is the plant pathology, and that the tree health care is a promising business for young plant pathology people, Korean Society of Plant Pathology is ought to be actively involved in the preparation of the enforcement ordinances and regulations, and help the early establishment of the new tree health care system in living spaces of Korea.

Thermal Design of MGSE Panel for Thermal Vacuum Test of Ka-band Engineering Qualification Model Payload of Communications and Broadcasting Satellite (통신방송위성 Ka-대역 기술인증모델 탑재체의 열진공시험을 위한 MGSE 패널 열설계)

  • Kim, Jeong Hun;Choe, Seong Bong;Yang, Gun Ho
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.31 no.2
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    • pp.96-102
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    • 2003
  • The thermal design of MGSE(Mechanical Ground Support Equipment) panel is performed for thermal vacum thest of Ka-band EQM(Engineering Qualification Model) payload of communications and broadcasting satellite. The thermal environments are predicted to evaluate the performance of transponder equipments in the thermal vacum chamber. SINDA is used to verify the thermal design of the heat pipe layout. Embedded 16 heat pipes in the EQM payload developed for Ka-band trasponder equipments are designded properly. The heat fluz loaded on the external facesheet is 265W/㎡ for the hot platear function test of the traspinder equipments, and the zero heat flux for the cold plateau case. The maxium predicted heat transport capability is 2723 W-cm.

A Gigabit Serial Transceiver Design Using FPGA for Satellite Communication Transponder (위성통신 중계기에서의 FPGA를 이용한 Gigabit 시리얼 송수신기 설계)

  • Hong, Keun-Pyo;Lee, Jung-Sub;Jin, Byoung-Il;Ko, Hyun-Suk;Seo, Hak-Geum
    • The Journal of Korean Institute of Communications and Information Sciences
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    • v.39A no.8
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    • pp.481-487
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    • 2014
  • In this paper, we have proposed gigabit serial transceiver based on backplane architecture at the satellite communication digital transponder. The transponder supports the full combinational switching function with broadband multi-channel using programmable device - Xilinx space-grade Virtex-5 FPGA. In order to implement the switching function, GTX transceiver solution inside Virtex-5 FPGA is used. Also hardware implementation is simple because of no additional component. In order to use a GTX transceiver, signal integrity(SI) simulation of PCB design is essential. We investigate the characteristics of the S-parameter, eye diagram, channel jitter of GTX transmission line and conform that GTX Transceiver operates without error. Finally the proposed PCB design will be utilized at satellite communication digital transponder EQM-2(Engineering Qualification Model-2).

Design Verification of Thermal Control Subsystem for EOS-C Ver.3.0 using STM Thermal Vacuum Test Result (STM 열진공 시험 결과를 이용한 EOS-C Ver.3.0 열제어계 설계 검증)

  • Chang, Jin-Soo;Yang, Seung-Uk;Jeong, Yun-Hwang
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.38 no.12
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    • pp.1232-1239
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    • 2010
  • A high-resolution electro-optical camera (EOS-C Ver.3.0), the mission payload of an Earth observation satellite, is under development in Satrec Initiative. We designed this system to give improved thermal performance compared with the EOS-C Ver.2.0 which is the main payload of DubaiSat-1 by optimizing the active and passive thermal control design. We developed the Structural-Thermal Model (STM) and verified the design margin by performing the qualification level thermal vacuum test. We also conducted the verification of its Thermal Mathematical Model (TMM) through the thermal balance test. As a result, it was confirmed that TMM faithfully represents the thermal characteristics of the EOS-C Ver.3.0.

RESEARCH FOR ROBUSTNESS OF THE MIRIS OPTICAL COMPONENTS IN THE SHOCK ENVIRONMENT TEST (MIRIS 충격시험에서의 광학계 안정성 확보를 위한 연구)

  • Moon, B.K.;Kanai, Yoshikazu;Park, S.J.;Park, K.J.;Lee, D.H.;Jeong, W.S.;Park, Y.S.;Pyo, J.H.;Nam, U.W.;Lee, D.H.;Ree, S.W.;Matsumoto, Toshio;Han, W.
    • Publications of The Korean Astronomical Society
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    • v.27 no.3
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    • pp.39-47
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    • 2012
  • MIRIS, Multi-purpose Infra-Red Imaging System, is the main payload of STSAT-3 (Korea Science & Technology Satellite 3), which will be launched in the end of 2012 (the exact date to be determined) by a Russian Dnepr rocket. MIRIS consists of two camera systems, SOC (Space Observation Camera) and EOC (Earth Observation Camera). During a shock test for the flight model stability in the launching environment, some lenses of SOC EQM (Engineering Qualification Model) were broken. In order to resolve the lens failure, analyses for cause were performed with visual inspections for lenses and opto-mechanical parts. After modifications of SOC opto-mechanical parts, the shock test was performed again and passed. In this paper, we introduce the solution for lens safety and report the test results.

The Study on the Implementation and Design of Power Supply Unit of Digital of Dehop/Rehop Transponder of EQM (우주 인증용 대전자전중계기의 전원공급기 설계 및 구현에 대한 연구)

  • Kim, Ki-Jung
    • The Journal of the Korea institute of electronic communication sciences
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    • v.16 no.3
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    • pp.437-442
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    • 2021
  • This study describes the design and implementation of power supply of dehop/rehop transponder of EQM(Engineering Qualification Model). We materialized the interface of the PLDIU and power supply of a satellite bus, and minimized the potential for the occurrence of such erroneous operation circuit ESD through the WCA of the space environment. We designed a reliable power supply through simulation for TID about space radiation and simulation of the vibration generated during it launched, and we confirmed that it satisfies the environmental test specification through the test space environment after production.

IRF Analysis Considering Clutter Background for SAR Image Qualification

  • Jung, Chul-H.;Oh, Tae-B.;Song, Sun-H.;Kwag, Young-K.
    • International Journal of Aeronautical and Space Sciences
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    • v.10 no.1
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    • pp.83-90
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    • 2009
  • A new IRF (Impulse Response Function) analysis technique in high resolution SAR image is presented by taking into account the real clutter environment. In order to investigate the realistic effect of clutter background on the impulse response function of SAR image, an ideally generated impulse response function is superimposed with a large number of background clutter data which are extracted from the various regions of an actual SAR image. As a performance measure, PSLR (Peak Sidelobe Ratio) of the clutter-contained IRF is presented in the various groups of clutter background, and finally the results are compared with the stochastic model.

과학위성 1호 종합 조립시험 구성

  • 신구환;이현우;박홍영;김경희;임종태
    • Bulletin of the Korean Space Science Society
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    • 2003.10a
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    • pp.51-51
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    • 2003
  • 인공위성의 개발 단계는 Prototype Model(PM), Engineering Model(EM), Qualification Model(QM) 그리고 Flight Model(FM)로 구분된다. 이때, Prototype 개발을 제외한 EM, QM, FM 개발단계는 반드시 종합조립시험(AIT)을 통하여 System Integration Test를 수행한다. 이 중에서 위성발사 전 최종 종합조립시험단계인 FM AIT는 위성의 최종시험단계이므로 Scenario Test를 포함한 지상에서 수행하여야 할 모든 시험을 수행한다. 이때, EM, QM 단계와는 다르게 FM AIT는 전기적 및 기계적 시험을 수행하나, 본 논문에서는 전기적 시험 과정과, Control Center 구성도 등을 포함하고 있는 Hardware 부분과, 관련 시험을 수행하게 될 Simulator를 포함한 Software 부분으로 나누어 소개하며, 기타 FM AIT 수행에 필요한 Electrical Ground Support System (EGSE) 전체 구성을 소개한다.

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