V26 传感元件 标准查询与下载

GB/T 41209-2021 月球与行星探测激光测距仪通用规范

本文件规定了应用于月球与行星探测任务的激光测距仪的技术要求、试验方法、包装、运输、存储和随行文件。 本文件适用于月球与行星探测任务的激光测距仪的设计、生产与应用等。其他工作于大气层外环境的激光测距仪参照使用。

General specifications for laser rangefinder for lunar and planetary exploration

ISO 8056-2:1988/Amd 1:2016 航空器.镍铬和镍铝热电偶的延伸电缆.第2部分:端头.一般要求和试验.修改件1

Aircraft - Nickel-chromium and nickel-aluminium thermocouple extension cables - Part 2: Terminations - General requirements and tests; Amendment 1

EN 4701-001:2014 航空航天系列.连接器，光学，矩形，模块化，工作温度125°.第001部分:技术规范

This European Standard specifies the general characteristics, the conditions for qualification, acceptance and quality assurance, as well as the test programs and groups for EN 4165 rectangular connectors with removable optical modules using EN 4531-101 contacts.

Aerospace series - Connectors@ optical@ rectangular@ modular@ operating temperature 125 �� for EN 4531-101 contacts - Part 001: Technical specification

EN 3375-012:2013 航空航天系列.数字数据传输用电缆.第012部分:单股.星绞100 ohms.260℃.KH型.产品标准

This European Standard specifies the dimensions, tolerances, required characteristics and the mass of an AWG 24 shielded quad cable, type KH, intended for high speed (100 Mbit/s) full duplex Ethernet networks. Linked to this particular application, the operating temperatures of the cable are between - 65 °C and 260 °C. This cable is laser markable, this marking satisfies the requirements of EN 3838. The characteristics impedance must be (100 ± 15).

Aerospace series - Cable@ electrical@ for digital data transmission - Part 012: Single braid - Star Quad 100 ohms - 260 ��- Type KH - Product standard

DIN EN 4645-002:2010 航空航天系列.光学圆型单芯和多芯连接头,螺纹环耦合,自锁定式1.25 mm直径金属包头,带可移动校准套筒支架的连接器.第002部分:触点配置和性能规范.德文和英文版本EN 4645-002-2009

Aerospace series - Connectors, optical, circular, single and multipin, coupled by threaded ring, self-locking 1,25 mm diameter ferrule with removable alignment sleeve holder - Part 002: Specification of performance and contact arrangements; German and Eng

GJB 6395-2008 航天器星敏感器通用规范

本规范规定了航天器星敏感器的技术要求、质量保证过和交货准备等。 本规范适用于航天器星敏感器（以下简称星敏感器）的设计、生产、检验和验收。

General specification for star sensor of spacecraft

DLA QPL-15160-69-2007 仪器引线.电力电话.一般规格

This list has been prepared for use by or for the Government in the acquisition of products covered by Specification MIL-PRF-15160. Listing of a product is not intended to and does not connote endorsement of the product by the Department of Defense. All products listed herein have been qualified under the requirements for the product as specified in the latest effective issue of the applicable specification. This list is subject to change without notice; revision or amendment of this list will be issued as necessary. The listing of a product does not release the supplier from compliance with the specification requirements.

FUSES, INSTRUMENT, POWER, AND TELEPHONE GENERAL SPECIFICATION FOR

HJB 368-2006 舰空导弹武器系统红外跟踪器通用规范

General specification for infrared tracker of ship-to-air missile weapon system

ARMY A-A-52567 B-2006 测量仪器:整体自动[代替:军用 MIL-S-0053085 A CANC 注意1.军用 MIL-S-53085.军用 MIL-S-0053085 A(1).军用 MIL-S-0053085 A]

The General Services Administration has authorized the use of this commercial item description for all federal agencies. The original issue of this CID replaced MIL-S-0053085A(ME)

SURVEY INSTRUMENT, AUTOMATED, INTEGRATED (AISI) [Replaced: ARMY MIL-S-0053085 A CANC NOTICE 1, ARMY MIL-S-53085, ARMY MIL-S-0053085 A (1), ARMY MIL-S-0053085 A]

DIN EN 2591-6305:2003 航空航天系列.光电连接件.试验方法.第6305部分:光学元件.温度急剧变化

The document specifies a method of checking the ability of optical connection elements (including permanent connections) and fibre optic couplers to withstand rapid changes of temperature such as might occur during transportation and in operation. It shall be used together with EN 2591.

Aerospace series - Elements of electrical and optical connection; Test methods - Part 6305: Optical elements; Rapid change of temperature; German and English version EN 2591-6305:2001

ARMY A-A-52575 A-2003 测量仪器-经纬仪.指示方向.一阶使用附件.三脚架和箱子

This document covers two types of illuminated, first-order theodolites with accessories, cases, and tripod.

THEODOLITES, SURVEYING, DIRECTION, FIRST-ORDER WITH ACCESSORIES, TRIPOD, AND CASES

QJ 3158-2002 地(舰)面用红外位标器通用规范

General specification for infrared localizer on ground and warship

SAE AS5392-2002 卫生和用途监控系统,转动系统检索式传感器规范

This SAE Aerospace Standard (AS) specifies requirements for the interface between a rotational system indexing sensor and its interface electronics. These sensors generate one or more electrical pulses for each revolution of the shaft being monitored. These pulses can be used to determine the actual shaft rotational speed and/or position for use in a Health and Usage Monitoring System (HUMS). Indexing sensors are used in the following HUMS areas on the aircraft: (a) rotor track and balance, (b) engine vibration monitoring and diagnostics, (c) drive train vibration monitoring and diagnostics. The goal of this standardization effort is to be able to take any compliant indexing sensor and connect it to any compliant interface electronics. These SAE HUMS Interface Specifications include the minimal interface and performance requirements for interoperability with the Rotorcraft Industry Technology Association (RITA) compliant HUMS. Compliance with these Interface Specifications can be referenced in more comprehensive procurement and device specifications.

Health and Usage Monitoring System, Rotational System Indexing Sensor Specification

AIR FORCE DI-QCIC-81611-2001 精密测量仪器实验室(PMEL)质量指南

This Data Item Description (DID) contains the format and content preparation instructions for the data product generated by the specific and discrete task requirement as delineated in the contract.

PRECISION MEASUREMENT EQUIPMENT LABORATORY (PMEL) QUALITY MANUAL

QJ 28A-1998 压力传感器静态性能不确定度计算方法

Calculation Method of Static Performance Uncertainty of Pressure Sensor

ARMY MIL-C-14806 A NOTICE 2-1997 玻璃仪器外壳及光楔用降低反射涂层

MIL-C-14806A dated 12 June 1969 with Amendment 2, dated 1 May 1974 and Validation notice 1, dated 15 May 1987 is inactive for new design and is no longer used, except for replacement purposes.

COATING, REFLECTION REDUCTING, FOR INSTRUMENT COVER GLASSES AND LIGHTING WEDGES

ITU-R RS.1281 FRENCH-1997 保护无线电定位服务中的电台免受 13.4-13.75 GHz 频段有源星载传感器的辐射

This Recommendation was jointly developed by Radiocommunication Study Groups 7 and 8, and future revisions should be undertaken jointly.

PROTECTION OF STATIONS IN THE RADIOLOCATION SERVICE FROM EMISSIONS FROM ACTIVE SPACEBORNE SENSORS IN THE BAND 13.4-13.75 GHz

ITU-R RS.1282 FRENCH-1997 在 1 260 MHz 附近风廓线雷达和有源星载传感器之间共享的可行性

active spaceborne sensors operate in the 1 215 to 1 300 MHz radiolocation band under the provision of No. S5.333 of the Radio Regulations

FEASIBILITY OF SHARING BETWEEN WIND PROFILER RADARS AND ACTIVE SPACEBORNE SENSORS IN THE VICINITY OF 1 260 MHz

ITU-R RS.1280 SPANISH-1997 选择有源星载传感器发射特性以减轻对在 1-10 GHz 频段运行的地面雷达产生干扰的可能性

active spaceborne sensors may be operated in common frequency bands with systems in the radiolocation and radionavigation services

SELECTION OF ACTIVE SPACEBORNE SENSOR EMISSION CHARACTERISTICS TO MITIGATE THE POTENTIAL FOR INTERFERENCE TO TERRESTRIAL RADARS OPERATING IN FREQUENCY BANDS 1-10 GHz

ITU-R RS.1281 SPANISH-1997 保护无线电定位服务中的电台免受 13.4-13.75 GHz 频段有源星载传感器的辐射

This Recommendation was jointly developed by Radiocommunication Study Groups 7 and 8, and future revisions should be undertaken jointly.

PROTECTION OF STATIONS IN THE RADIOLOCATION SERVICE FROM EMISSIONS FROM ACTIVE SPACEBORNE SENSORS IN THE BAND 13.4-13.75 GHz