SAE AIR 744C-2010
航空辅助电源

Aerospace Auxiliary Power Sources


SAE AIR 744C-2010 发布历史

This SAE Aerospace Information Report (AIR) is a review of the general characteristics of power sources that may be used to provide secondary, auxiliary, or emergency power for use in aircraft, space vehicles, missiles, remotely piloted vehicles, air cushion vehicles, surface effect ships, or other vehicles in which aerospace technology is used. The information contained herein is intended for use in the selection of the power source most appropriate to the needs of a particular vehicle or system. The information may also be used in the preparation of a power source specification. Considerations for use in making a trade study and an evaluation of the several power sources are included. More detailed information relating to specific power sources is available in other SAE Aerospace Information Reports or in Aerospace Recommended Practices.

SAE AIR 744C-2010由美国机动车工程师协会 US-SAE 发布于 2010-06-16。

SAE AIR 744C-2010 在中国标准分类中归属于: V40 电气系统与设备,在国际标准分类中归属于: 49.080 航空航天用流体系统和零部件。

SAE AIR 744C-2010 发布之时,引用了标准

* 在 SAE AIR 744C-2010 发布之后有更新,请注意新发布标准的变化。

SAE AIR 744C-2010的历代版本如下:

SAE AIR 744C-2010 由 SAE AIR 744B-1995 变更而来。

 

 

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标准号
SAE AIR 744C-2010
发布日期
2010年06月16日
实施日期
废止日期
中国标准分类号
V40
国际标准分类号
49.080
发布单位
US-SAE
引用标准
ASTM D 910-2007 ASTM D 1655-2009 ASTM D 1655-2010 MIL-PRF-7808-1997 MIL-PRF-23699-1997 MIL-STD-810-2008 RTCA DO-178B-1992 RTCA DO-254-2000 RTCA DO-311-2008 SAE AIR 1168/1-1989 SAE AIR 1343A-1992 SAE J 1775-2004 SAE ARP 699E-1997 DOT 3HT MIL-DTL-5624
被代替标准
SAE AIR 744B-1995
适用范围
This SAE Aerospace Information Report (AIR) is a review of the general characteristics of power sources that may be used to provide secondary, auxiliary, or emergency power for use in aircraft, space vehicles, missiles, remotely piloted vehicles, air cushion vehicles, surface effect ships, or other vehicles in which aerospace technology is used. The information contained herein is intended for use in the selection of the power source most appropriate to the needs of a particular vehicle or system. The information may also be used in the preparation of a power source specification. Considerations for use in making a trade study and an evaluation of the several power sources are included. More detailed information relating to specific power sources is available in other SAE Aerospace Information Reports or in Aerospace Recommended Practices.




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