V70 航天器综合 标准查询与下载

BS EN 14777:2004 航天工程.Multipaction设计和试验

This document specifies the requirements and recommendations for the design and test of RF components and equipment to achieve acceptable performance with respect to multipaction-free operation in service in space. The document includes: — verification planning requirements; — definition of a route to conform to the requirements; — design and test margin requirements; — design and test requirements; and — informative annexes that provide guidelines on the design and test processes. This document is intended to result in the effective design and verification of the multipaction performance of the equipment and consequently in a high confidence in achieving successful product operation. This document covers multipaction events occurring in all classes of RF satellite components and equipment at all frequency bands of interest. Operation in single carrier CW and pulse modulated mode are included, as well as multi-carrier operations. This document does not include breakdown processes caused by collisional processes, such as plasma formation. This document is applicable to all space missions. When viewed in a specific project context, the requirements defined in this document should be tailored to match the genuine requirements of a particular profile and circumstances of a project. NOTE Tailoring is a process by which individual requirements of specifications, standards and related documents are evaluated and made applicable to a specific project, by selection and in some exceptional cases, modification of existing or addition of new requirements.

Space engineering - Multipaction design and test

ISO 15864:2004 空间系统.航空器、子系统和装置的一般试验方法

This International Standard provides the baseline standard on the subject of testing at the system, subsystem and unit levels for applicable unmanned spacecraft programmes. It also provides the requirements for documentation associated with testing activities. The acceptance criteria, specifications or procedures, and other detail test requirements applicable to a particular programme are defined in the applicable technical specifications and statement of work. When requirements have to be verified by measuring product performance and function under various simulated environments, the method is referred to as "Test". The requirements of this International Standard may be tailored for each specific space programme application.

Space systems - General test methods for space craft, subsystems and units

BS ISO 16458:2004 航天系统.无人宇宙飞船运输.通用要求

This International Standard is applicable to unmanned spacecraft and their supporting hardware including science instrument and payloads. It establishes the requirements for transportation by rail, road, air, and water and as a part of a launch vehicle and establishes the requirements for special containers and loading/unloading operations meant to safeguard unmanned spacecraft and their supporting hardware during transportation. This International Standard is intended to be applied in international transportation. It may also be used in national transportation.

Space systems - Unmanned spacecraft transportation - General requirements

BS ISO 14950:2004 航天系统.无人宇宙飞船的可操作性

This International Standard defines the essential properties pertaining to the operation of unmanned spacecraft and defines requirements and guidelines for spacecraft on-board functions in order to enable a specified ground segment to operate the spacecraft in any nominal or predefined contingency situation.

Space systems - Unmanned spacecraft operability

DLA A-A-59199 VALID NOTICE 1-2004 光学透镜洗涤剂(准备使用)

A-A-59199, dated 12 May 1998, has been reviewed and determined to be valid for use in acquisition

CLEANING COMPOUND, OPTICAL LENS (READY TO USE)

ISO 14950:2004 航天系统.不载人航天器的可操作性

This International Standard defines the essential properties pertaining to the operation of unmanned spacecraft and defines requirements and guidelines for spacecraft on-board functions in order to enable a specified ground segment to operate the spacecraft in any nominal or predefined contingency situation.

Space systems - Unmanned spacecraft operability

AIR FORCE MIL-STD-1821 NOTICE 3-2004 标准模拟器数据库交替模式

MIL-STD-1821, dated 17 June 1993, is inactive for new design and shall be no longer used for new designs.

STANDARD SIMULATOR DATA BASE (SSDB) INTERCHANGE FORMAT (SIF)

QJ 3189-2004 靶场技术问题处理规定

Regulations on Handling Technical Issues in the Shooting Range

QJ 3191-2004 地（舰）空导弹遥测系统设计要求

Design Requirements for Surface (Ship) Air Missile Telemetry System

ISO 17399:2003 空载系统.载人系统集成

This International Standard defines all generic requirements for manned space flight vehicle/habitat structures and flight crew training or simulation facilities and the related equipment that directly interfaces with manned space system flight crew members. This International Standard covers the field of human factors as they relate to the space environment and space habitats. These man–systems integration requirements are applicable to space system launch, re-entry, on-orbit and extraterrestrial environments. The requirements specified herein are applicable to new manned space flight programmes and projects.

Space systems - Man-systems integration

KS W 0622-2003 飞机的强度和刚度.地面试验

이 규격은 비행기의 구조를 평가하기 위하여 필요한 지상 시험에 대하여 규정한다. 이 중

Airplane strength and rigidity ground tests

KS W 0624-2003 飞机的强度和刚度.振动

1.1 이 규격은 다음 사항에 대하여 규정한다.a) 비행기의 설계와 제조에서 구조의 진

Airplane strength and rigidity vibration

DLA MIL-DTL-3661 C-2003 通用技术条件指示灯镜头指示灯支架指示灯灯座

This specification covers the general requirements for lampholders, indicator lights, indicatorlight housings, and indicator-light lenses including display and integral lamp driver network types and associated hardware. For the purpose of this specification, an indicator-light housing is an indicator light without a lens (see 6.5).

LAMPHOLDERS, INDICATOR LIGHTS, INDICATOR LIGHT HOUSINGS, AND INDICATOR LIGHT LENSES, GENERAL SPECIFICATION FOR

DLA MIL-DTL-3661 C SUPP 1C-2003 通用技术条件指示灯镜头指示灯支架指示灯灯座

This supplement forms a part of MIL-DTL-3661C, dated 10 JUNE 2003.

LAMPHOLDERS, INDICATOR LIGHTS, INDICATOR LIGHT HOUSINGS, AND INDICATOR LIGHT LENSES, GENERAL SPECIFICATION FOR

QJ 3167-2003 运载火箭低温贮箱共底真空性能测试方法及安全监测要求

Test method and safety monitoring requirements for common-bottom vacuum performance of low-temperature storage tanks of launch vehicles

DLA MIL-DTL-32134-2003 眼镜保持皮带

This document covers the requirements for an eyewear retention strap to be used with the Advanced Combat Helmet (ACH)

STRAP, EYEWEAR, RETENTION

QJ 3182-2003 液体火箭发动机总体检漏方法

General Leak Detection Method for Liquid Rocket Engine

KS W 0623-2002 飞机的强度和刚度.抖晃、发散及其他空气弹性力上的不稳定

1.1 일 반 이 규격은 다음 항목에 대한 일반적 사항에 대하여 규정한다.a)비행기

Airplane strength and rigidity, flutter, divergence,and other aeroelastic instabilities

KS W 0614-2002 航空器气压系统的设计及安装标准

이 규격은 항공기 공기압 계통의 설계 및 장착의 일반적 사항에 대하여 규정한다. 여기에는

Design, installation, and data requirements for pneumatic systems, aircraft

DLA MS23006 VALID NOTICE 2-2002 飞行器航空和警告灯罩

MS23006, dated 28 JULY 1964, has been reviewed and determined to be valid for use in acquisition.

COVER, LIGHT, NAVIGATIONAL AND WARNING, AIRCRAFT