V15 复合材料与固体燃料 标准查询与下载

DLA MS9483 REV B NOTICE 1-2000 直式管装-AMS5646钎焊套圈

This notice should be filed in front of MS9483B, dated 1 May 1969. MS9483B is inactive for new design and is no longer to be used except for replacement purposes.

FERRULE, BRAZING, TUBE FITTING-AMS5646, STRAIGHT

AECMA PREN 3102-2000 航空航天系列密封剂　试验方法 低温挠性的确定

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 AECMAMembers. It has been technically approved by the experts of the concerned Technical Committee following comment by the Member countries.

Aerospace Series Sealants Test Methods Determination of Low-Temperature Flexibility Edition P 1

ARMY A-A-51461 C-2000 凝固点和亚硝酸盐浓度抗冻测试条和彩色图表的检测试剂盒

This commercial item description(CID) covers the requirements fi tem description, r test kits suitable ~ for determining the freezing point and reserve alkalinity of ethylene glycol antifreeze solutions as well as both the universal freezing point and nitrite concentration of multi engine type antifreeze solutions used in engine cooling systems.

TEST KIT, TEST STRIPS AND COLOR CHART, ANTIFREEZE, FREEZE POINT AND NITRITE CONCENTRATION

AECMA PREN 3361-2000 航空航天系列.消耗电极再熔炼固溶处理和沉淀处理FE-PM1802(X5CrNiCu15-5)钢　薄板和带材a小于或等于6 mm 、 1070 MPa小于或等于Rm小于或等于1220MPa

This standard specifies the characteristics of screws, 100°countersunk normal head, offset cruciform recess, threaded to head, in alloy steel, cadmium plated.

Aerospace Series Steel FE-PM1802 (X5CrNiCu15-5) Consumable Electrode Remelted Solution Treated and Precipitation Treated Sheet and Strip a Less Than or Equal to 6 mm 1 070 MPa Less Than or Equal to Rm Less Than or Equal to 1 220 MPa Edition P 3

AECMA PREN 3364-2000 航空航天系列.消耗电极再熔炼软化的FE-PM1802(X5CrNiCu15-5)钢锻坯a或直径D小于或等于300 mm

This standard defines terms for optical fibres and cable.

Aerospace Series Steel FE-PM1802 (X5CrNiCu15-5) Consumable Electrode Remelted Softened Forging Stock a or D Less Than or Equal to 300 mm Edition P 3

DLA MIL-DTL-29181C NOTICE 1-2000 [代替: 国防后勤局 军事标准-H-43905 C CANC 注意 2, 国防后勤局 军事标准-H-43905 C 注意 1, 国防后勤局 军事标准-H-43905 C, 国防后勤局 军事标准-H-43905 B, 国防后勤局 军事标准-H-43905 A, 国防后勤局 军事标准-H-43905]重型及中型安全挂锁高覆盖搭扣

The General Services Administration has authorized the use of this commercial item description as a replacement for Military Specifications MIL-V-16720E and MIL-V-16721D which are cancelled.

HASP, HIGH SECURITY, SHROUDED, FOR HIGH AND MEDIUM SECURITY PADLOCK [Superseded: DLA MIL-H-43905 C CANC NOTICE 2, DLA MIL-H-43905 C NOTICE 1, DLA MIL-H-43905 C, DLA MIL-H-43905 B, DLA MIL-H-43905 A, DLA MIL-H-43905]

DLA A-A-59530 A-2000 8英寸长安全靴

This commercial item description covers the requirements for an aircrew safety boot.

BOOT, SAFETY, (8 INCH)

AECMA PREN 3748-2000 航空航天系列Ｏ形环尺寸.P1版

This ’Xerospace 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 AECMAMembers. It has been technically approved by the experts of the concerned Technical Committee following commenf by the Member countries.

Aerospace Series O-Ring Grooves Dimensions Edition P 1

DLA A-A-59123-2000 工业重铬酸钠二水合物 [代替:DLA O-S-595 B CANC 通告 1,DLA O-S-595 B(1),DLA O-S-595 B,DLA O-S-595 A(3),DLA O-S-595 A,DLA O-S-595]

This commercial item description (CID) covers technical grade sodium dichromate

SODIUM DICHROMATE DIHYDRATE, TECHNICAL [Superseded: DLA O-S-595 B CANC NOTICE 1, DLA O-S-595 B (1), DLA O-S-595 B, DLA O-S-595 A (3), DLA O-S-595 A, DLA O-S-595]

ARMY MIL-E-255 A VALID NOTICE 1-2000 乙基固体燃料稳定剂(二乙二苯基脲)

MIL-E-255A(i>, dated 8 June 1966, has been reviewed and determined to be valid for use pri acquisition.Custodiam:k ~- A~R y Navy - os DEA - GS Preparing

ETHYL CENTRALITE (CARBAMITE)

NAVY QPL-8605-20-2000 裂化重油用纤维素醋酸丙酸酯

This list has been prepared for use by or for the Government in the acquisition of products covered by the subject specification and such listing of a product is not intended to and does not connote endorsement of the product by the Department of Defense.

CAP, PRESSURE FUEL SERVICING

DLA OO-W-2803 NOTICE 1-2000 平底船的安全型手摇滚筒式绞车

This notice should be filed in front of OO-W-2803, dated November 23, 1992.

WINCHES, DRUM, HAND-OPERATED, SAFETY TYPE, FOR PONTOON BARGES

DLA A-A-59621-2000 醋酸黑色围巾[取代:海军MIL-N-87042 C,海军 MIL-N-87042 B,海军 MIL-N-87042 A(2),海军 MIL-N-87042 A(1),海军 MIL-N-87042 A,海军 MIL-N-87042]

The General Services Administration has authorized the use of this commercial item description as a replacement for Military Specifications MIL-V-16720E and MIL-V-16721D which are cancelled.

NECKERCHIEF (ACETATE BLACK) [Superseded: NAVY MIL-N-87042 C, NAVY MIL-N-87042 B, NAVY MIL-N-87042 A (2), NAVY MIL-N-87042 A (1), NAVY MIL-N-87042 A, NAVY MIL-N-87042]

ISO 14951-7:1999 航天系统 流体特性 第7部分:肼推进剂

This part of ISO 14951 specifies limits for the chemical composition and physical properties of hydrazine (N2H4) propellant and test methods for verification of propellant composition. This part of ISO 14951 is applicable to hydrazine propellant of the following grades, intended for use as a fuel in propellant systems of space systems: — standard: normal production and quality control (suitable for most uses); — monopropellant: normal product with strict control of specified impurities (to be specified only for monopropellant catalytic engines where extended life of the catalyst is desired); — high purity: special production with strict control of specified impurities. This part of ISO 14951 is applicable to propellant used in both flight hardware and ground facilities, systems, and equipment. It is applicable to influents only to the extent specified herein. CAUTION — Hydrazine, in the liquid or vapour form, is toxic and volatile. Care should be taken in the handling and storage of hydrazine to prevent contact with the human body and with materials that are not compatible.

Space systems - Fluid characteristics - Part 7: Hydrazine propellant

ISO 14951-6:1999 航天系统 流体特性 第6部分:一甲基肼推进剂

This part of ISO 14951 specifies limits for the composition of monomethylhydrazine (N2H3CH3) (MMH) propellant and test methods for verification of propellant composition. This part of IS014951 is applicable to monomethylhydrazine propellant of the following grades, intended for use as a fuel in propellant systems of space systems: — grade A: 98,0 % pure; — grade F: 98,5 % pure. This part of ISO 14951 is applicable to propellant used in both flight hardware and ground facilities, systems, and equipment. It is applicable to influents only to the extent specified herein. CAUTION — Monomethylhydrazine, in the liquid or vapour form, is toxic and volatile. Care should be taken in the handling and storage of monomethylhydrazine to prevent contact with the human body and with materials that are not compatible.

Space systems - Fluid characteristics - Part 6: Monomethylhydrazine propellant

ISO 14951-5:1999 航天系统 流体特性 第5部分:四氧化二氮推进剂

This part of ISO 14951 specifies limits for the chemical composition and physical properties of N2O4 propellant and test methods for verification of propellant composition. This part of ISO 14951 is applicable to N2O4 propellant of the following types and grades, intended for use as an oxidizer in propellant systems of space systems: — types — NTO: nominal 99,5 % N2O4 purity with red-brown colour; — MON-1: nominal 99 % N2O4 and 1 % NO with green colour; — MON-3: nominal 97 % N2O4 and 3 % NO with green colour; — MON-10: nominal 90 % N2O4 and 10 % NO with green colour; — MON-25: nominal 75 % N2O4 and 25 % NO with green colour; — grades: — standard: no iron requirement; — low-iron: 0,5 μg/g iron maximum. This part of ISO 14951 is applicable to propellant used in both flight hardware and ground facilities, systems, and equipment. It is applicable to influents only to the extent specified herein. CAUTION — Nitrogen tetroxide, in the liquid or vapour form, is toxic and volatile. Care should be taken in the handling and storage of nitrogen tetroxide to prevent contact with the human body and with materials that are not compatible.

Space systems - Fluid characteristics - Part 5: Nitrogen tetroxide propellant

ISO 14951-8:1999 航天系统 流体特性 第8部分:煤油推进剂

This part of ISO 14951 specifies limits for the composition of kerosene propellant intended for use as a fuel for propellant systems of space systems, and test methods for verification of propellant composition. This part of ISO 14951 is applicable to propellant used in both flight hardware and ground facilities, systems, and equipment. This part of ISO 14951 applies to influents only to the extent specified herein.

Space systems - Fluid characteristics - Part 8: Kerosene propellant

NAVY MIL-T-29586 (1)-1999 (宽度达60英寸)单向碳纤维增强预浸带热固性聚合物基体的一般规格

This amendment forms ap art of MIL-T-29586(AS), dated 30 April 1991 , and is approved for use by the Naval Air Systems Command, Departmento f the Navy,a nd is available for use by all Departments and Agencies of the Department of Defense

THERMOSETTING POLYMER MATRIX, UNIDIRECTIONAL CARBON FIBER REINFORCED PREPREG TAPE (WIDTHS UP TO 60 INCHES), GENERAL SPECIFICATION FOR

ARMY MIL-A-192 B VALID NOTICE 2-1999 高氯酸铵

MIL-A-192B, dated 10 April 1986, has been reviewed and determined to be valid for use in acquisition.

AMMONIUM PERCHLORATE

DLA MS51526 REV A NOTICE 1-1999 37度扩口式O形圈直管轴套适配器

This notice should be filed in front of MS51526A, dated 17 January 1979.

ADAPTER, STRAIGHT, TUBE TO BOSS, O-RING, 37 DEGREE FLARED (LONG) [Refer To: SAE J514, SAE J514, SAE J514, SAE J514, SAE J514]