共找到 73 条与 传感元件 相关的标准,共 5 页
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
Aircraft - Nickel-chromium and nickel-aluminium thermocouple extension cables - Part 2: Terminations - General requirements and tests; Amendment 1
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
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
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
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
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
General specification for infrared tracker of ship-to-air missile weapon system
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]
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
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
General specification for infrared localizer on ground and warship
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
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
Calculation Method of Static Performance Uncertainty of Pressure Sensor
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
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
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
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
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
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