V10 航空、航天材料基础标准 标准查询与下载

ASTM F1362-97 航天工业用上釉叠层材料的剪切强度和剪切模数测试方法

1.1 This test method is used to determine the shear strength and shear modulus of interlayer materials that are restrained by relatively high modulus plies in laminated transparencies. This test method can be used with single or multiple plies of the same interlayer materials. 1.2 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use. 1.3 The values stated in SI units are to be regarded as the standard. The values in parentheses are for information only.

Standard Test Method for Shear Strength and Shear Modulus of Aerospace Glazing Interlayer Materials

AECMA PREN 4381-1997 航空航天系列.抗热合金NI-PH3601(NiCr22Mo9Nb)溶液处理无缝管道结构应用3mm小于或等于直径D小于或等于50mm.P1版

This standard is initially published on green paper for the needs of AECMA-Members (Association Europeenne des Constructeurs de Matdriel Adrospatial). it has been technically approved by the experts of the concerned AECMA Commission following comment by the manufacturers of the Member countries.

Aerospace Series Heat Resisting Alloy NI-PH3601 (NiCr22Mo9Nb) Solution Treated Seamless Tubes for Structural Application D Less Than or Equal to 50 mm, a Less Than or Equal to 3 mm Edition P 1

AECMA PREN 4380-1997 航空系列 抗热合金NI-PH3601(NiCr22Mo9Nb)溶液处理锻造小于或等于200mm.P1版

This "Aerospace Series" Prestandard ,,as been drawn up under the responsibility of AECMA-STAN (The European Association of Aerospace Industries - Standardization). It is published on green paper for the needs of the European Aerospace Industry. It has been technically approved by the experts of the concerned Domain following member comments.

Aerospace Series Heat Resisting Alloy NI-PH3601 (NiCr22Mo9Nb) Solution Treated Bar and Section De Less Than or Equal to 200 mm Edition P 1

AECMA PREN 4379-1997 航空系列 抗热合金NI-PH3601(NiCr22Mo9Nb)溶液处理锻造小于或等于200mm.P1版

This "Aerospace Series" Prestandard has been drawn up under the responsibility of AECMA (The European Association of Aerospace Industries). it is published on green paper for the needs of AECMA-Members. It has been technically approved by the experts of the concerned Technical Committee following comment by the Member countries.

Aerospace Series Heat Resisting Alloy NI-PH3601 (NiCr22Mo9Nb) Solution Treated Forging De Less Than or Equal to 200 mm Edition P 1

ARMY MIL-C-10382 D NOTICE 2-1997 应用于食物装卸机械和设备的喷雾喷涂矿脂防腐剂

This notice should be filed in front of MILC l0382D, dated 6 October 1983.

CORROSION PREVENTIVE, PETROLATUM, SPRAYING APPLICATION: FOR FOOD HANDLING MACHINERY AND EQUIPMENT

AECMA PREN 4377-1997 航空系列 抗热合金NI-PH2601(NiCr19Fe19Nb5Mo3)非热处理锻造或直径D小于或等于300mm.P1版

This "Aerospace Series" Prestandard has been drawn up under the responsibility of AECMA (The European Association of Aerospace Industries). it is published on green paper for the needs of AECMA-Members. It has been technically approved by the experts of the concerned Technical Committee following comment by the Member countries.

Aerospace Series Heat Resisting Alloy NI-PH2601 (NiCr19Fe19Nb5Mo3) Non Heat Treated Forging Stock a or D Less Than or Equal to 300 mm Edition p 1

AECMA PREN 4376-1997 航空系列 抗热合金NI-PH2601(NiCr19Fe19Nb5Mo3)溶液处理杆剖面直径D小于或等于200mm.P1版

This standard is part of the series of EN metallic material standards for aerospace applications. The general organization of this series is described in EN 4258. This standard has been prepared in accordance with EN 4500-2.

Aerospace Series Heat Resisting Alloy NI-PH2601 (NiCr19Fe19Nb5Mo3) Solution Treated and Precipitation Treated Bar and Section De Less Than or Equal to 200 mm Edition P 1

AECMA PREN 4375-1997 航空系列 抗热合金NI-PH1301(NiCr19Co18Mo4Ti3Al3)非热处理锻造或直径D小于或等于250mm.P1版

This standard specifies the characteristics of jam-nuts for jam-nut receptacles in the family of circular electrical connectors coupled by threaded ring.

Aerospace Series Heat Resisting Alloy NI-PH1301 (NiCr19Co18Mo4Ti3Al3) Non Heat Treated Forging Stock a or D Less Than or Equal to 250 mm Edition P 1

AECMA PREN 4374-1997 航空系列 抗热合金NI-PH1301(NiCr19Co18Mo4Ti3Al3)溶液处理杆剖面小于或等于200mm.P1版

This "Aerospace Series" Prestandard has been drawn up under the responsibility of AECMA (The European Association of Aerospace Industries). it is published on green paper for the needs of AECMA-Members. It has been technically approved by the experts of the concerned Technical Committee following comment by the Member countries.

Aerospace Series Heat Resisting Alloy NI-PH1301 (NiCr19Co18Mo4Ti3Al3) Solution Treated and Precipitation Treated Bar and Section De Less Than or Equal to 200 mm Edition P 1

AECMA PREN 4373-1997 航空系列 抗热合金NI-PD9001(NiCu31)焖火无缝管3mm小于或等于直径D小于或等于75mm.P1版

This standard is part of the series of EN metallic material standards for aerospace applications. The general organization of this series is described in EN 4258. This standard has been prepared in accordance with EN 4500-3.

Aerospace Series Heat Resisting Alloy NI-PD9001 (NiCu31) Annealed Seamless Tube D Less Than or Equal to 75 mm, a Less Than or Equal to 3 mm Edition P 1

AECMA PREN 4370-1997 航空系列 抗热合金NI-PH1701(NiCr15Co14Al5Ti4Mo4)非热铸造或直径D小于或等于100mm.P1版

This standard specifies the characteristics of elbow, 37°in titanium alloy intended for use in aircraft fluid system pipe lines.

Aerospace Series Heat Resisting Alloy NI-PH1701 (NiCr15Co14Al5Ti4Mo4) Non Heat Treated Forging Stock a or D Less Than or Equal to 100 mm Edition P 1

AECMA PREN 4369-1997 航空系列 抗热合金NI-PH1701(NiCr15Co14Al5Ti4Mo4)溶液处理杆剖面直径D小于或等于100mm.P1版

This standard is part of the series of EN metallic material standards for aerospace applications. The general organization of this series is described in EN 4258. This standard has been prepared in accordance with EN 4500-3.

Aerospace Series Heat Resisting Alloy NI-PH1701 (NiCr15Co14Al5Ti4Mo4) Solution Treated and Precipitation Treated Bar and Section De Less Than or Equal to 100 mm Edition P 1

AECMA PREN 4368-1997 航空系列 抗热合金NI-CD1701(NiCo15Cr10Al6Ti5Mo3)非热熔化.P1版

This standard specifies the required characteristics for lamp, code 718, used on-board aircraft. It shall be used together with EN 2756.

Aerospace Series Heat Resisting Alloy NI-CD1701 (NiCo15Cr10Al6Ti5Mo3) Non Heat Treated Remelting Stock Edition P 1

AECMA PREN 4315-1997 航空系列 抗热合金FE-PA2601(X6NiCrTiMoV26-15)溶液处理和杆剖面或直径D小于或等于100mm Rm≥900 Mpa.P1版

This standard is part of the series of EN metallic material standards for aerospace applications. The general organization of this series is described in EN 4258. This standard has been prepared in accordance with EN 4500-3.

Aerospace Series Heat Resisting Alloy FE-PA2601 (X6NiCrTiMoV26-15) Solution Treated and Precipitation Treated Bar and Section a or D Less Than or Equal to 100 mm Rm Greater Than or Equal to 900 MPa Edition P 1

AECMA PREN 4314-1997 航空系列 抗热合金FE-PA2602(X4NiCrTiMoV26-15)非热螺纹锻造或直径D小于或等于250mm.P1版

This standard is part of the series of EN metallic material standards for aerospace applications. The general organization of this series is described in EN 4258. This standard has been prepared in accordance with EN 4500-3.

Aerospace Series Heat Resisting Alloy FE-PA2602 (X4NiCrTiMoV26-15) Non Heat Treated Forging Stock a or D Less Than or Equal to 250 mm Edition P 1

ARMY MIL-C-60251 A (5)-1997 M80型7.62MM北约球状炮弹的间接火力运用

This amendment forms a part of MIL-C-60251A(MU), dated 05 March 1971, and is approved for use by the US Army Armament, Research, Development and Engineering Center, and is available for use by all Departments and Agencies of the Department of Defense.

CARTRIDGE, 7.62MM, NATO, BALL, M80 OVERHEAD FIRE APPLICATION

ARMY MIL-C-60252 A (5)-1997 M62型7.62MM北约示踪剂炮弹的间接火力运用

This amendment forms a part of MIL-C-60252A(MU), dated 30 April 1971, and is approved for use by the US Army Armament, Research, Development and Engineering Center, and is available for use by all Departments and Agencies of the Department of Defense.

CARTRIDGE, 7.62MM, NATO, TRACER, M62 OVERHEAD FIRE APPLICATION

ARMY MIL-C-46281 F (3)-1997 M62型7.62MM北约示踪剂弹筒

This amendment forms a part of MIL-C-46281F(AR), dated 24 November 1987, and is approved for use by the US Army Armament, Research, Development and Engineering Center, and is available for use by all Departments and Agencies of the Department of Defenie.

CARTRIDGE, 7.62MM, NATO, TRACER, M62

ARMY MIL-C-50704 A (2)-1997 XM276型7.62MM.微光曳光弹

This amendment forms a part of MIL-C-50704A, dated 20 September 1991, and is approved for use by the US Army Armament, Research, Development and Engineering Center, and is available for use by all Departments and Agencies of the Department of Defense.

CARTRIDGE, 7.62MM: DIM TRACER, XM276

NAVY MIL-STD-176 A NOTICE 1-1997 导弹和航天发射车载重和平衡数据报告表格

MIL-STD-l76A, dated 27 May 1963, is inactive for new design. Refer to the Department of Defense Adopted, Society of Allied Weight Engineers (SAW). Recommended Practice No.1 O, “Weight and Balance Data Reporting Forms for Guided Missiles and Space Launch Vehicles,” for new design.

GUIDED MISSILES AND SPACE LAUNCH VEHICLES, WEIGHT AND BALANCE DATA REPORTING FORMS FOR