V04 基础标准与通用方法 标准查询与下载

ISO 21460:2007 空间数据和信息传输系统.接近1的空间链接协议.物理层

This International Standard defines the Proximity-1 space link protocol physical layer. It specifies the channel connection process, provision for frequency bands and assignments, hailing channel, polarization, modulation, data rates, and performance requirements. Currently, the physical layer only defines operations at UHF frequencies for the Mars environment. The coding layer is defined in ISO 21459. The data link layer is defined in ISO 22663. This International Standard does not specify a) individual implementations or products; b) implementation of service interfaces within real systems; c) the methods or technologies required to perform the procedures; or d) the management activities required to configure and control the protocol. The scope and field of application are furthermore detailed in subclause 1.3 of the enclosed CCSDS publication.

Space data and information transfer systems - Proximity-1 space link protocol - Physical layer

GJB 1124A-2007 握杆操纵中手部数据和手指功能

本标准规定了握杆操纵飞机飞行员的手部数据和手指功能。 本标准适用于歼击机、强击机、歼击轰炸机及上述飞机的教练机中央驾驶杆、侧驾驶杆、油门杆的设计。

The data of hands and the function of fingers in hands on throttle and stick (HOTAS)

DIN EN 4179:2007 航空航天系列.无损检验人员的资格和认可

This standard establishes the minimum requirements for the qualification and certification of personnel involved in non-destructive testing(NDT).These requirements include training,experience and examinations for personnel performing NDT in the aerospace manufacturing,service,maintenance and overhaul industries.

Aerospace series - Qualification and approval of personnel for non-destructive testing; German and English version EN 4179:2005

BS ISO 11078:2007 飞行器.解冻液/防冰液.ISO II型、III型和IV型

This International Standard defines the requirements for non Newtonian ISO types II, III and IV fluids used in the removal and prevention of ice, snow, or frost on exterior surfaces of main line and regional civil transport airplanes on the ground. This International Standard is applicable to de-icing/anti-icing fluids for use on airplanes in general. However, the applicability may have limitations for particular airplane types. It is the airplane operator’s responsibility to consult the aircraft operations manual, the aircraft maintenance manual and the service letters of the airplane manufacturer, to determine any limitations/restrictions relating to the use of de-icing/anti-icing fluids that conform to this International Standard for the type and model of airplane to be treated. See also ISO 11076.

Aircraft - De-icing/anti-icing fluids - ISO type II, III and IV

BS ISO 11075:2007 飞行器.解冻液/防冰液.ISO I型

This International Standard defines the requirements for ISO type I fluids used in the removal and prevention of ice, snow, or frost on exterior surfaces of main line and regional civil transport airplanes on the ground. This International Standard is applicable to de-icing/anti-icing fluids for use on airplanes in general. However, the applicability may have limitations for particular airplane types. It is the airplane operator’s responsibility to consult the aircraft operations manual, the aircraft maintenance manual and the service letters of the airplane manufacturer, to determine any limitations/restrictions relating to the use of de-icing/anti-icing fluids that conform to this International Standard for the type and model of airplane to be treated. See also ISO 11076.

Aircraft - De-icing/anti-icing fluids - ISO type I

ISO 21349:2007 航天系统.规划评定

This International Standard provides process requirements for project reviews as a set of required functions. The requirements and recommendations cover the function inputs, outputs, mechanisms and controlling conditions. It is intended for use in implementing the review requirements of ISO 14300-1, ISO 14300-2, ISO 15865 and such other space systems and operations standards that require formal reviews. This International Standard specifies the responsibilities of a review board and gives guidance concerning review board composition. This International Standard is applicable to reviews for a project at any level within a larger project, as well as for major milestone reviews at the top level of a major project. It is intended to be used either by an independent developer as a basis for enterprise processes, or as a basis for an agreement between a supplier and a customer. This International Standard also provides normative descriptions of the kinds of reviews that are commonly useful in assuring the success of a space project.

Space systems - Project reviews

KS W ISO 1151-5:2007 飞行力学.概念、量和符号.第5部分:测量用的物理量

KS W ISO 1511의 이번 부에서는 비행측정에서 사용되는 물리량들을 다룬다.ISO

Flight dynamics-Concepts, quantities and symbols-Part 5:Quantities used in measurements

KS W ISO 1151-1:2007 飞行力学.概念、量和符号.第1部分:航空器相对于空气的运动

KS W ISO 1511의 이번 부에서는 기본 정의와 지구에 대해서 상대적으로 일정한 속도

Flight dynamics-Concepts, quantities and symbols-Part 1:Aircraft motion relative to the air

NAVY QPL-85052-9 NOTICE 1-2007 有垫层环状夹一般规定

The preparing activity above was responsible for this document as of the date shown above. Since organizations and responsibilities can change, you should verify the currency of the information above using the ASSIST Online database at http://assist.daps.dla.mil.

CLAMP, LOOP, CUSHION, GENERAL SPECIFICATION FOR

KS W ISO 9031:2007 航空货运设备.集装单元装置(ULDs)的装运系统.图形符号

이 규격은 단위적재장치에 대한 항공기 화물 취급 시스템의 그림 표시를 위한 기호를 규정한다

Air cargo equipment-Handling systems for unit load devices(ULDs)-Symbols for pictorial representation

SAE AS94900-2007 航空航天飞行控制系统设计、安装和军用飞行器试飞行的通用规范

This specification establishes general performance, design, test, development and quality assurance requirements for the Flight Control Systems of military piloted aircraft. Flight Control Systems (FCS) include all components used to transmit flight control commands from the pilot or other sources to appropriate force and moment producers. Flight control commands normally result in control of aircraft altitude, airspeed, flight path, attitude, aerodynamic or geometric configuration, ride quality, and structural modes. Among components included are the pilot's controls, dedicated displays and logic switching, system inertial and air data sensors, signal computation, test devices, mechanical transmission devices, actuators, power sources, and signal transmission lines dedicated to flight control. Excluded are aerodynamic surfaces, engines and engine control systems, rotorcraft rotors, fire control devices, crew displays and electronics not dedicated to flight control. In the event of conflict between this specification and other referenced documents, this specification shall govern. The detail requirements for a particular system shall be specified in the FCS Specification, 4.6.2, the Aircraft Detail Specification, the contract, or purchase order for that system. Most of the technical concepts and approaches covered by the document represent industry "best practice". They are based on sound and proven engineering practices and have demonstrated successful production experience. Others require specific approval from the procuring activity before use. This requirement for approval is not intended to prohibit their use; but rather to ensure that the prime contractor has fully investigated their capability to perform reliably and to be sufficiently durable under the required conditions and that the prime contractor can present substantiating evidence for approval before the design is committed to.

Aerospace - Flight Control Systems - Design, Installation and Test of Piloted Military Aircraft, General Specification For

SAE ARP5945-2007 飞机除冰/防冰液 SAE I 型的耐久时间测试

The purpose of this ARP is to provide the sample selection criteria and test procedures for SAE Type I aircraft deicing/anti-icing fluids, required for the generation of endurance time data of acceptable quality for review by the SAE G-12 Holdover Time Subcommittee. A significant body of previous research and testing has indicated that all Type I fluids formulated with glycol perform in a similar manner from an endurance time perspective. This applies to Type I deicing/anti-icing fluids formulated with propylene glycol, ethylene glycol, and diethylene glycol only. Type I deicing/anti-icing fluids containing these glycol bases no longer require testing for endurance times. The methods described in this ARP shall be employed, however, if endurance time testing of a glycol-based Type I deicing/anti-icing fluid is desired or requested by a fluid manufacturer, operator or other organization. Fluids formulated with glycol bases other than those listed herein, and all non-glycol Type I deicing/anti-icing fluids, must be tested for endurance times using the methods described in this ARP (as appropriate).

Endurance Time Tests for Aircraft Deicing/Anti-icing Fluids SAE Type I

SAE AMS1424H-2007 除冰/防冰液，飞机，SAE 1 类

This specification covers a deicing/anti-icing material in the form of a fluid. The fluid is generally used heated either diluted with water, or as supplied, for the removal of, and time-limited protection against, deposits of frost, ice, and snow on exterior aircraft surfaces prior to takeoff. Consult aircraft manufacturer's maintenance manual and service letters to determine any restrictions relating to the use of deicing/anti-icing fluids for type and model of aircraft being treated. Refer also to SAE ARP 4737. The manufacturer shall determine and report the lowest operational use temperature (LOUT) for the recommended dilutions of their fluid(s). The LOUT for an SAE Type I fluid is the lowest temperature at which the fluid has been tested and certified in accordance with the appropriate aerodynamic acceptance tests (3.5.3) while maintaining the 10 °C (18 °F) freezing point buffer (see SAE ARP 4737).

Deicing/Anti-Icing Fluid, Aircraft, SAE Type 1

SAE AIR5704-2007 稠化的航空器防冻液用现场粘度试验

This SAE Aerospace Information Report (AIR) provides a description of a screening method for use in the field for verifying an AMS 1428 anti-icing fluid is above its minimum low shear viscosity as published with holdover time guidelines. The test will determine if the fluid is (a) satisfactory, (b) unsatisfactory, or (c) borderline needing more advanced viscometry testing. Other field tests may be required to determine if an anti-icing fluid is useable, such as refractive index, appearance or other tests as may be recommended by the fluid manufacturer.

Field Viscosity Test for Thickened Aircraft Anti-Icing Fluids

SAE AMS1428F-2007 流体，飞机除冰/防冰，非牛顿，（假塑料），SAE II、III 和 IV 类

This specification covers three types of deicing/anti/icing material, each in the form of a non-Newtonian fluid.

Fluid, Aircraft Deicing/Anti-Icing, Non-Newtonian, (Pseudoplastic), SAE Types II, III, and IV

SAE ARP5485A-2007 飞机除冰/防冰液 SAE II、III 和 IV 类耐久时间测试

The purpose of this SAE Aerospace Recommended Practice (ARP) is to provide the sample selection and endurance time test procedures, for SAE Type II, III, and IV aircraft deicing/anti-icing fluids, required for the generation of endurance time data of acceptable quality for review by the SAE G-12 Holdover Time Subcommittee.

Endurance Time Tests for Aircraft Deicing/Anti-Icing Fluids SAE Type II, III, and IV

SAE AIR825/2-2007 急性高度照射对人体的影响:生理学保护要求

The intent of this SAE Aerospace Information Report (AIR) is to describe the effects of the environmental changes on human physiology and the protection required to avoid negative consequences resulting from altitude exposure. A brief presentation of basic terms and considerations required to discuss the topic of human physiology at altitude are followed by an overview of the cardiovascular and respiratory systems. Issues specifically related to human exposure to altitude are then discussed. Hypoxia, hyperventilation, barotrauma, and decompression sickness (DCS) are each addressed: hypoxia is defined as an insufficient supply of oxygen to the tissues, hyperventilation is an excessive rate of ventilation with ultimate consequences on acido-basic equilibrium, barotrauma is injury caused by pressure: most commonly referencing injury to the walls of the Eustachian tube and the ear drum due to the difference between atmospheric and intratympanic pressures, and DCS is related to an excess of nitrogen in the body tissues. One goal of this AIR is to demonstrate the necessity of oxygen use for prevention of physical and psychological problems, or loss of consciousness in an aircraft pilot, flight crew, or passengers. Hopefully, this will provide a clear understanding as to why the use of supplemental oxygen is required for flight crew and passengers at altitudes greater than 12,000 ft (3650 m).

Effects of Acute Altitude Exposure in Humans: Requirements for Physiological Protection

SAE AS5900B-2007 (R) SAE AMS 1424 和 SAE AMS 1428 飞机除冰/防冰液空气动力学验收的标准测试方法

This SAE Aerospace Standard (AS) establishes the aerodynamic flow-off requirements for SAE AMS 1424 Type I and SAE AMS 1428 Type II, III and IV fluids used to deice and/or anti-ice aircraft: a. with takeoff rotation speeds generally exceed approximately 100 knots, with time from brake release to rotation speed greater than 20 s, typical for large transport type jet aircraft. This procedure is referred to as the High Speed Ramp Test. and/or b. with takeoff rotation speeds generally exceed approximately 60 knots, with time from brake release to rotation speed greater than 15 s typical for commuter type aircraft. This procedure is referred to as the Low Speed Ramp Test. The objective of this standard is to ensure acceptable aerodynamic characteristics of the deicing/anti-icing fluids as they flow off aircraft lifting and control surfaces during the takeoff ground acceleration and climb.

(R) Standard Test Method for Aerodynamic Acceptance of SAE AMS 1424 and SAE AMS 1428 Aircraft Deicing/Anti-icing Fluids

DIN EN 9133:2007 航空航天系列.质量管理体系.航空航天标准部件的合格测试程序

This document provides a basic uniform method for ensuring that aerospace standard parts(products) conform with the requirements of technical specifications referring to qualified parts and for a manufacturer of such parts to have a qualified management system at least equivalent to EN 9100． EN 9100 and EN 9103 apply when called out in the aerospace standard part standard.

Aerospace series - Quality management systems - Qualification procedure for aerospace standard parts; German and English version EN 9133:2004

ISO/TR 23462:2007 航天系统.航天规划管理框架的定义指南

This Technical Report provides a framework within which an organization can establish the basis for the development of programme/project management specifications and plans when undertaking the execution of a specific programme/project. It enables the programme/project manager to establish the criteria for programme/project success and to secure the organization’s commitment to the programme/project manager’s management approach for the overall programme/project and its constituent elements. It includes guidelines leading to the establishment of a programme/project management framework, and identification of practices to be applied. Following these guidelines also results in traceability of the considerations and decisions on why and how the programme/project is conducted according to its specific characteristics. This Technical Report provides a holistic approach for programme/project managers to apply their organization's programme/project management practices when defining the management framework for programme/project planning. It is based on a systematic method of defining the programme/project objectives and success criteria, identifying and elaborating the specific characteristics of their programme/project, specifying the management elements needed, establishing and agreeing the management approaches to be implemented, compiling these into a programme/project management framework document. The guidelines in this Technical Report are applicable to any organization undertaking the execution of space programmes/projects.

Space systems - Guidelines to define the management framework for a space project