共找到 1494 条与 机上设备和仪器 相关的标准,共 100 页
This standard specifies a method of determining the tensile strength test for short length of optical fibre.It shall be used together with EN 2591-100.
Aerospace series - Fibres and cables, optical, aircraft use - Test methods - Part 502: Tensile stength for short length of optical fibres
This standard specifies three methods of checking the effectiveness of cable attachment in the cyclic flexing mode for optical connection elements (including permanent connections) and fibre optic couplers.It shall be used together with EN 2591-100.
Aerospace series - Elements of electrical and optical connection - Test methods - Part 609: Optical elements - Effectiveness of cable attachment - Cable cyclic flexing
This standard specifies a method to determine the effects of thermal shock on an optical fibre or cable.
Aerospace series - Fibres and cables, optical, aircraft use - Test methods - Part 404: Thermal shock
Specification and test requirements for a single-axis Coriolis vibratory gyro (CVG) for use as a sensor in attitude control systems, angular displacement measuring systems, and angular rate measuring systems are defined. A standard specification format guide for the preparation of a single-axis CVG is provided. A compilation of recommended procedures for testing a CVG, derived from those presently used in the industry, is also provided. Informative annexes cover CVG design features and theoretical principles of operation.
IEEE Standard Specification Format Guide and Test Procedure for Coriolis Vibratory Gyros
This standard establishes baseline requirements for the design, fabrication, test, inspection, storage, and transportation of a flywheel rotor assembly used in a spaceflight flywheel system for energy storage and/or attitude control. These requirements when implemented on a particular system will assure a high level of confidence in achieving safe and reliable operation
Space Systems - Flywheel Rotor Assemblies
This slash sheet specifies the operational parameters and characteristics of a particular implementation of the SAE Linear, Token Passing Bus (LTPB) Interface Unit. This slash sheet defines the following: a. the physical media interface: this slash sheet specifies the characteristics of the optical interface to the physical bus media; b. the minimum and maximum timing requirements for operation of this implementation of the LTPB; c. the data coding used to encode and decode the data for transmission; and d. the default values to be loaded into the timers of the LTPB interface at power-up prior to intervention by the host processor.
Type F-1 Fiber Optic Media Interface Characteristics
This standard was developed under the auspices of the CEA R-7.1 Home Control Systems Subcommittee.
Tunneling Device Area Network Protocols Over Internet Protocol Channels
この規格は,主として民間航空機及び輸送機に用いる搭載機器の種々の環境条件及び試験手順について規定する。
Aircraft -- Environmental conditions and test procedures for airborne equipment
この規格は,航空機搭載機器(以下,搭載機器又は単に機器ともいう。)に対する一連の最低標準環境試験条件(カテゴリ)及び適用試験手順について規定する。
Airborne equipment -- Environmental conditions and test procedures
This list has been prepared for use by or for the Government in the acquisition of products covered by the subject specification and such listing of a product is not intended to and does not connote endorsement of the product by the Department of Defense.
INDICATOR, PRESSURE, HYDRAULIC, 0-4,000 PSI
This list has been prepared for use by or for the Government in the acquisition of products covered by the subject specification and such listing of a product is not intended to and does not connote endorsement of the product by the Department of Defense.
INDICATOR, PRESSURE, OIL, 0-100 PSI
This list has been prepared for use by or for the Government in the acquisition of products covered by the subject specification and such listing of a product is not intended to and does not connote endorsement of the product by the Department of Defense.
INDICATOR, PRESSURE, HYDRAULIC, 0-4,000 PSI INTEGRALLY LIGHTED
This manual provides information to manufacturers of cathode ray tube products on how to comply with the U.S.Food and Drug Administration requirements for x-radiation emissions. It is meant to serve as a training manual for people who are responsible for this compliance and not as an official CDRH published guideline.
CRT X-Radiation Compliance Training Manual
A-A-52508A, dated 18 November 1996, has been reviewed and determined to be valid for use in acquisition
INDICATOR, VOLTAGE: BATTERY-GENERATOR, 28 VOLT DC (NOMINAL) (METRIC)
This Commercial Item Description (CID), details requirements for furnishing and installing a commercially available precision Roundness and Geometry Measuring System (RGMS).
GAGE, COMPARATOR, ELECTRIC
This list has been prepared for use by or for the Government in the acquisition of products covered by the subject specification and such listing of a product is not intended to and does not connote endorsement of the product by the Department of Defense.
INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, CYLINDER HEAD, 0 DEG. C TO 300 DEG. C
This list has been prepared for use by or for the Government in the acquisition of products covered by the subject specification and such listing of a product is not intended to and does not connote endorsement of the product by the Department of Defense.
INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED
This SAE Aerospace Information Report (AIR) provides methodologies and approaches that have been used to install and integrate full-authority-digital-engine-control (FADEC) systems on transport category aircraft. Although the information provided is based on turbofan engines installed on large commercial transports, many of the issues raised are equally applicable to corporate, general aviation, regional and commuter aircraft, and to military installations, particularly when commercial aircraft are employed by military users. The word ?engine? is used to designate the aircraft propulsion system. The engine station designations used in this report are shown in Figure 1. Most of the material concerns an Electronic Engine Control (EEC) with its associated software, and its functional integration with the aircraft. However, the report also addresses the physical environment associated with the EEC and its associated wiring and sensors. Since most of today?s transport category engines use dual-channel full-authority digital engine control (FADEC) systems, this is the configuration which is primarily addressed. A typical FADEC system configuration is shown in Figure 2. Special considerations that pertain to single-channel FADEC systems or limited authority ?supervisory? control systems are also addressed.
Guidelines for the Integration of Electronic Engine Control Systems with Transport Category Aircraft Systems
This ARP covers three common lamp light sources, incandescent, electroluminescent and light emitting diode that, when NVG filtered, can be used to illuminate NVG compatible aerospace crew stations. It is recognized that many other different light sources can also be used for this purpose. This ARP sets forth recommendations for the design of NGV compatible lighting, utilizing these light sources, that will meet the requirements of MIL-L-85762A Lighting, Aircraft, Interior, Night Vision Imaging System (NVIS) Compatible. Although this ARP concentrates on lamp light sources for illumination, the information contained within this ARP may be directly applied to incandescent, electroluminescent and light emitting diode information display devices. This SAE Aerospace Recommended Practice recommends certain basic considerations which the design engineer should observe when designing NVG compatible lighting.
Night Vision Goggle (NVG) Compatible Light Sources
MS24576B remains inactive for new design, however, the document is valid for acquisition without change.
INDICATOR, PRESSURE OIL
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