SAE AMS2505 Aluminum Paint Finishing, Low Baking (Cancelled Dec 2008)
作者:标准资料网 时间:2024-05-10 23:44:22 浏览:8173
来源:标准资料网
Product Code:SAE AMS2505
Title:Aluminum Paint Finishing, Low Baking (Cancelled Dec 2008)
Issuing Committee:Ams B Finishes Processes And Fluids Committee
Scope:This specification has been declared 驴CANCELLED驴 by the Aerospace Materials Division, SAE, as of December 2008. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been 驴CANCELLED驴.
MIL-HDBK-762, MILITARY HANDBOOK: DESIGN OF AERODYNAMICALLY STABILIZED FREE ROCKETS (17 JUL 1990)., This chapter introduces the handbook. Rocket systems are presented in two broad classes: military rocket systems and research rocket systems. Military rocket systems are discussed in terms of their application in a battle environment. Research rocket systems are discussed in terms of the application to provide the means of placing data gathering equipment into a desired environment. Operational modes for the rocket systems are described. Finally, brief descriptions of the remaining chapters and the appendices are given. Aerodynamically stabilized free rockets offer relatively simple, reliable, small, low-cost means for delivering payloads and, when great accuracy is not required, are often the optimum systems. This handbook provides engineering design information and data for such rockets. Primarily, this handbook is intended to cover the conceptual and preliminary design phases; however, reference is made to the technical approaches and computer programs required for the system development phase. The material includes operational and interface requirements as they influence the design of the total weapon system. The handbook provides 1. The preliminary design engineer with specific design information and data useful in the rapid response situations required of preliminary design activities 2. The specialist in each technical area an introduction to the other disciplines in terms of data requirements and trade-off studies that must be performed. Free flight rockets are those rockets that do not have an in-flight guidance system; they are aimed, guided, or directed by the launching device. These launchers usually have a launching rail or tube to provide initial direction to the rocket. Free flight rockets are of two basic kinds?spin stabilized and aerodynamically stabilized. The spin stabilized rocket, as the name implies, depends upon a high rate of spin and resulting gyroscopic moments to oppose disturbances. The aerodynamically stabilized rocket depends upon aerodynamic forces on the body and fins to oppose disturbing forces. The aerodynamically stabilized rocket generally employs some spin to minimize dispersion caused by nonsymmetrical body characteristics (body asymmetries, fin misalignment, thrust misalignment, etc.). The data and concepts presented in this handbook are limited to aerodynamically stabilized free flight rockets.
基本信息
| 标准名称： | 饲料添加剂 大豆磷脂 |
| 英文名称： | Feed additive—Soybean lecithin |
| 中标分类： |
农业、林业 >>
畜牧 >>
畜禽饲料与添加剂 |
| ICS分类： |
农业 >>
饲料
|
| 发布部门： | 中华人民共和国国家质量监督检验检疫总局 中国国家标准化管理委员会 |
| 发布日期： | 2009-05-26 |
| 实施日期： | 2009-10-01 |
| 首发日期： | 2009-05-26 |
| 作废日期： | |
| 主管部门： | 中华人民共和国国家质量监督检验检疫总局 |
| 提出单位： | 全国饲料工业标准化技术委员会 |
| 归口单位： | 全国饲料工业标准化技术委员会 |
| 起草单位： | 上海市饲料质量监督检验站、上海市农业科学院农产品质量标准与检测技术研 |
| 起草人： | 赵志辉、杨海锋、顾赛红、林淼、黄志英、凤懋熙 |
| 出版社： | 中国标准出版社 |
| 出版日期： | 2009-10-01 |
| 页数： | 12页 |
| 计划单号： | 20071210-T-469 |
适用范围
本标准规定了饲料添加剂大豆磷脂产品的技术要求、试验方法、检验规则及标签、包装、运输、贮存。
本标准适用于从大豆中提取的，用作饲料添加剂的大豆磷脂产品.
前言
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目录
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引用标准
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所属分类： 农业 林业 畜牧 畜禽饲料与添加剂 农业 饲料
