SAE AS 47641-1999
MIL-STD-1760B飞机挂点接口确认方法

Validation Methods for MIL-STD-1760B Aircraft Station Interfaces

SAE AS 47641-1999 发布历史

This document establishes techniques for validating that an Aircraft Station Interface (ASI) complies with the interface requirements delineated in MIL-STD-1760B Notice 3. For validation of aircraft designed to MIL-STD-1760A Notice 2 AS4764 Issued 1995-04 applies. The purpose of this document is to provide methods for validating that an aircrafts store electrical interface complies with the aircraft station interface (ASI) requirements of MIL- STD-1760 Notice 3. This document provides a modular, independent set of methods for each of the requirements in MIL-STD-1760 that applies to aircraft requirements. The methods herein apply to the auxiliary (AUX) interface as well as the primary interface of MIL-STD-1760.

SAE AS 47641-1999由美国机动车工程师协会 US-SAE 发布于 1999-08-01。

SAE AS 47641-1999 在中国标准分类中归属于: V21 管件、卡箍、密封件，在国际标准分类中归属于: 35.200 接口和互连设备,49.020 航空器和航天器综合。

SAE AS 47641-1999 发布之时，引用了标准

• STANAG 3350-1995 
• SAE AS 4113-1989 数字式时分制指令/响应型多路传输数据总线控制器的验证测试计划

SAE AS 47641-1999的历代版本如下：

• 1999年08月01日 SAE AS 47641-1999 MIL-STD-1760B飞机挂点接口确认方法

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标准号

SAE AS 47641-1999

发布日期

1999年08月01日

实施日期

废止日期

无

中国标准分类号

V21

国际标准分类号

35.200;49.020

发布单位

US-SAE

引用标准

EIA-STD-RS-170 EIA-STD-RS-343-A STANAG 3350-1995 MIL-C-39029-1988 MIL-STD-1553-1978 SAE AS 4113-1989 ASD-TR-87-5028 MIL-A-8591 MIL-B-5087 MIL-C-38999 MIL-C-45662 MIL-E-6051 MIL-HDBK-235 MIL-HDBK-1553 MIL-STD-461 MIL-STD-462 MIL-STD-704 MIL-STD-1498 MIL-ST

适用范围

This document establishes techniques for validating that an Aircraft Station Interface (ASI) complies with the interface requirements delineated in MIL-STD-1760B Notice 3. For validation of aircraft designed to MIL-STD-1760A Notice 2 AS4764 Issued 1995-04 applies. The purpose of this document is to provide methods for validating that an aircrafts store electrical interface complies with the aircraft station interface (ASI) requirements of MIL- STD-1760 Notice 3. This document provides a modular, independent set of methods for each of the requirements in MIL-STD-1760 that applies to aircraft requirements. The methods herein apply to the auxiliary (AUX) interface as well as the primary interface of MIL-STD-1760.