CAJ | 학술논문

为满足在保证产品质量基础上缩短运载火箭型号研制周期的需要，根据并行工程思想提出了基于IPT的运载火箭研制模式，并在总结工程实践经验基础上对IPT运作原则、IPT组织与管理模式、基于技术成熟度的技术状态分级管理和基于PDM的IPT设计与制造协同模式进行了分析，为提高运载火箭产品研制效率提供了一种解决方案。
위만족재보증산품질량기출상축단운재화전형호연제주기적수요，근거병행공정사상제출료기우IPT적운재화전연제모식，병재총결공정실천경험기출상대IPT운작원칙、IPT조직여관리모식、기우기술성숙도적기술상태분급관리화기우PDM적IPT설계여제조협동모식진행료분석，위제고운재화전산품연제효솔제공료일충해결방안。
In order to meet both product quality requirement and shorter product development cycle time for launch vehicle, a IPT based development pattern is proposed in accordance with CE (Concurrent Engineering) IPT’s operation principles, organization and management pattern for IPT, classified management for technical status based on technology maturity and IPT’s col aboration paradigm between product design and manufacturing based on PDM are analyzed according to the summarized engineering and practical experiences. The proposed pattern offers a solution to improving launch vehicle development efficiency.