• 시스템엔지니어링학술지
• /
• 제10권2호
• /
• pp.89-95
• /
• 2014

In recent years, the United States have been several major failures of launch. As a result of these failures, activity of mission assurance valued. Mission assurance is defined as the application of systems engineering process towards the goal of achieving mission success. Therefore, mission assurance perform independent technical assessments throughout the concept and requirements definition, design, development, production, test, deployment, and operations phases. Space system program was emphasized the importance of the system engineering for that required huge cost and long term development. For this reason, independent review and verification of mission assurance is essential. Mission assurance gives us confidence to proceed with launch and best opportunity for mission success. In this study, framework of mission assurance is proposed by foreign case analysis.

• 항공우주시스템공학회지
• /
• 제9권2호
• /
• pp.41-46
• /
• 2015

The various risk factors that affected schedule, costs and mission success, etc. in development of the satellite. This paper derives the considerable "Cost of Quality" factors in the satellite development phase through the survey of practical techniques in respect of measurement of quality cost in the commercial products manufacturing, and proposes mitigation strategy of quality cost using the approach that can be minimized it.

• 항공우주시스템공학회지
• /
• 제12권5호
• /
• pp.76-88
• /
• 2018

미 항공우주국(NASA), 유럽우주기구(ESA) 등의 우주기관 및 미국 군에서는 제품보증 수행에 대한 요구조건 및 계획 등에 대한 가이드라인 또는 표준서를 제시하고 있다. 최근 들어, 세계의 주요 위성제작사는 테일러링(tailoring)을 통해 과도한 제품보증 요구조건 및 프로세스를 완화하고 있다. 비용 및 일정의 효율성을 증진시키기 위한 테일러링을 수행한다는 의미이다. 제품보증 테일러링은 임무, 임무 리스크의 유형, 복잡도, 개발비용 및 수명주기 등의 다양한 인자를 기준으로 수행될 수 있다. 본 연구에서는 NASA에서 제안된 임무 리스크(mission risk) 분류에 따른 제품보증 업무를 조사하고, 개발비용 및 일정의 최적화를 위한 테일러링 방안을 제시한다. 특히, 국내에서 개발하여 운용 중이거나 개발 중인 위성에 대한 임무 리스크 유형을 정의하고 이들에 대한 제품보증 특성을 비교 분석한다.

• 한국추진공학회지
• /
• 제2권2호
• /
• pp.108-117
• /
• 1998

엔진 내구성시험(AMT : Accelerated Mission Test : 또는 임무 가속시험) 기법을 이용한 엔진 부품의 국산화에 따른 품질 보증 시험이 수행되었다. 엔진 내구성시험 기법은 엔진의 개발/구성품 개량, 부품의 기술변경에 따른 인정시험이나, 입증시험을 위한 시험방법으로 1976년부터 적용되기 시작하였다. 본 논문은 국내에서 수행되었던 시험경험을 바탕으로 아직 국내에서 생소한 내구성시험에 대한 개념, 시험수행 절차와 방법 그리고 시험평가 수행 방안을 제시하였으며, 이를 통하여 엔진 부품의 국내 개발/생산시 품질인증을 위한 시험/평가 가능성을 제시하였다.

• 대한산업공학회지
• /
• 제41권2호
• /
• pp.144-149
• /
• 2015

In this study, the effective technology readiness assessment (TRA) method for system development project is suggested. We analyze the domestic and foreign TRA practice and derive the new idea to resolve the problems found from the analysis. Domestic and foreign organizations develop and use checklist for the precise TRA, but the checklist has some problems in type of questions and analysis of assessment. TRA method using the original TRL definition or the checklist should be selected depending on the project characteristic. Questions of the checklist should be classified into critical or non-critical according to their importance. Finally, Test and evaluation master plan (TEMP) in system engineering process can provide an obvious criteria to assess technology readiness level (TRL) of critical technology elements (CTE) composing the system.

• 한국항공우주학회지
• /
• 제43권2호
• /
• pp.156-165
• /
• 2015

궤도 속도에 근접하거나 궤도운동을 하고 있는 발사체 상단의 지구 재진입에 따른 지상피해 분석에 이용하기 위하여 지구 재진입 물체의 생존성 분석 프로그램(SAPAR: Survivability Analysis Program for Atmospheric Reentry)을 개발하였다. 3자유도 파편 낙하시뮬레이션 과정에 파편이 낙하하는 도중에 받게 되는 공력 열하중, 열하중에 의한 파편의 온도변화, 녹는점에 도달한 후 물체의 상변화 여부 등을 포함하여 최종적으로 지상에 낙하하는 파편의 크기와 무게를 분석하였다. 개발된 코드의 검증을 위하여 단순한 형태의 파편에 대한 생존성 분석을 수행하여 미항공우주국(NASA)과 유럽우주국(ESA)의 코드 결과와 비교하였다. 또한 실제 재진입 파편에 대한 분석을 수행하여 측정된 결과와 비교하였다.

• 항공우주시스템공학회지
• /
• 제3권1호
• /
• pp.6-11
• /
• 2009

It is anticipated that quality assurance for the Ka band Communication Payload System(COPS) development program of the communication, Ocean & Meteorological Satellite(COMS) may be a core technical factor to be concerned in order to avoid any failure, and to assure its final performance during the mission lifetime in space. Those can be managed and verified and assessed by performing the Quality Assurance (QA) and risk management which helps to prevent and to reduce the critical fails. This paper introduces the Product Assurance (PA) system and procedures for controlling and monitoring sub-contractors which were participated in Ka band Communication Payload System (COPS) development. Also this paper shows Quality Assurance (QA) procedures and detailed their processes for assured the product performed by local companies from site survey for selecting companies to delivery of their equipment.

• 항공우주시스템공학회지
• /
• 제2권1호
• /
• pp.22-27
• /
• 2008

It is anticipated that quality assurance for the Ka band Communication Payload System(COPS) development program of the Communication, Ocean & Meteorological Satellite(COMS) may be a core technical factor to be concerned in order to avoid any failure, and to assure its performance during the mission lifetime in space. Those can be managed and verified and assessed by performing the Quality Assurance (QA) and risk management which helps to prevent and reduce the critical fails. This paper introduces the Product Assurance (PA) system and procedures for Ka band Communication Payload System which was established and performed during the Qualification Model (QM) manufacturing phase. In this paper, we present detailed process for the products manufactured by local companies according to PA procedures operated through whole phases from design to test of equipment. Also this paper shows Quality Assurance (QA) procedures and detailed their processes for assured the product quality manufactured by local companies.

• International Journal of Computer Science & Network Security
• /
• 제22권12호
• /
• pp.146-152
• /
• 2022

The National Agency for Quality Assurance in Higher Education plays a crucial role in education in Ukraine, as an independent entity creates and ensures quality standards of higher education, which allow to properly implement the educational policy of the state, develop the economy and society as a whole. The purpose of the article: to reveal the crucial role of the National Agency for Quality Assurance in Higher Education to create quality management of higher education institutions, to show its mechanism as an independent entity that creates and ensures quality standards of higher education. and society as a whole. The mission of the National Agency for Quality Assurance in Higher Education is to become a catalyst for positive changes in higher education and the formation of a culture of its quality. The strategic goals of the National Agency are implemented in three main areas: the quality of educational services, recognition of the quality of scientific results, ensuring the systemic impact of the National Agency. The National Agency for Quality Assurance in Higher Education exercises various powers, which can be divided into: regulatory, analytical, accreditation, control, communication. The effectiveness of the work of the National Agency for Quality Assurance in Higher Education for 2020 has been proved. The results of a survey conducted by 183 higher education institutions of Ukraine conducted by the National Agency for Quality Assurance in Higher Education are shown. Emphasis was placed on the development of "Recommendations of the National Agency for Quality Assurance in Higher Education regarding the introduction of an internal quality assurance system." The international activity and international recognition of the National Agency for Quality Assurance in Higher Education are shown.

• 한국신뢰성학회지:신뢰성응용연구
• /
• 제4권2호
• /
• pp.105-119
• /
• 2004

Reliability program is essential to the development of space systems like launch vehicles and satellites, as they are non-repairable after launch and the failure of a launch vehicle resulted in catastrophic consequences for the mission. Foreign advanced space organizations have developed and implemented their own reliability management programs for launch vehicles from the conceptual design stage to the detail processes for the individual components, procedures and test reports. A study on the launch failures and the reliability analysis methods for one-shot devices contained in this paper will contribute to the reliability improvement for Korean launch vehicle and components.