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MIL-HDBK-336-2, MILITARY HANDBOOK SURVIVABILITY, AIRCRAFT, NONNUCLEAR, GENERAL CRITERIA (VOLUME 2) (21 SEP 1983)., This is the first volume in a four-volume design handbook for nonnuclear survivability of military aircraft. Each volume is structured to be used in conjunction with the other three volumes, as needed, in the design process. This volume contains specific subsystem design concepts, procedures, and other pertinent information. The information and design guidance contained in this volume is arranged in a manner to enhance its use in the conceptual design process, system research, design, test, and evaluation (RDT&E) programs, and existing aircraft modification programs where nonnuclear survivability features are required. Specific information pertinent to each subsystem is contained therein. This volume is arranged to permit the designer or analyst to select the specific area or subject of concern in the design or modification of an aircraft system and find the candidate design methods that may be considered for use. Table 1-1 is a matrix of the general survivability enhancement methods and the subsystems associated with military aircraft. The general applicability of the listed methods, for each subsystem, is indicated by a dot in the matrix. This serves as a preliminary check list for the user to ensure that all potential candidate survivability enhancement methods are considered. The use of this chart is an essential step in the process of selecting the most effective combination of survival enhancement features for the given aircraft design concept. APPLICATION: The data contained in this design handbook have been arranged to support the development of both fixed and rotary wing military aircraft. Each has unique mission and performance characteristics that require specialized attention and design solutions. The subystem design categories have been established with these considerations in mind. For example, the power train and rotor blade subsystems deal primarily with military helicopter applications, while the launch/recovery systems deal with those subsystem elements for both fixed and rotary wing aircraft landing gear systems and for those systems related to the assisted takeoff (launching) and deceleration (recovery) methods most used by the Air Force and Navy fixed-wing aircraft.

标准名称：	油气田集输工艺安装工程劳动定额
英文名称：	Labor quota for installation engineering of oil & gas gathering & transferring process
中标分类：	石油 >> 石油综合 >> 经济管理
ICS分类：	社会学、 服务、公司(企业)的组织和管理、行政、运输 >> 公司(企业)的组织与管理 >> 劳动资源管理
替代情况：	SY/T 5749-1995;被SY/T 5749-2012代替
发布部门：	国家发展和改革委员会
发布日期：	2004-07-03
实施日期：	2004-11-01
首发日期：	1900-01-01
作废日期：	2012-03-01
主管部门：	国家发展和改革委员会
提出单位：	石油工业劳动定员定额标准化技术委员会
归口单位：	石油工业劳动定员定额标准化技术委员会
起草单位：	中国石油天然气集团公司管道局
起草人：	李文华、张明生、吴晓林、陈国俊、刘春荣、杨斌
出版社：	石油工业出版社
出版日期：	2004-09-25
页数：	37页
批文号：	14047-2004
书号：	155021.5820

本标准是为满足石油行业油、气田地面建设施工生产的需要，在全面考虑了全国陆上各油、气田建设施工生产的特点和管理工作的情况的基础上编制的。本标准可作为油田建设企业内部组织生产、编制施工作业计划、签发施工任务书、考核工效、计算计件工资和奖金、进行经济核算的依据。

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