MIL-STD-2217 (NOTICE 1)
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MIL-STD-2217 (NOTICE 1), MILITARY STANDARD: MEMORY LOADER/VERIFIER MULTIPLEX BUS INTERFACE WITH AVIONIC SYSTEMS, REQUIREMENTS FOR (28 MAY 1993)., TO ALL HOLDERS OF MIL-STD-2217(AS): The following pages of MIL-STD-2217(AS) have been revised and supersede the pages listed.
MIL-STD-2217 (NOTICE 1)
MIL-STD-2217 (NOTICE 1), MILITARY STANDARD: MEMORY LOADER/VERIFIER MULTIPLEX BUS INTERFACE WITH AVIONIC SYSTEMS, REQUIREMENTS FOR (28 MAY 1993)., TO ALL HOLDERS OF MIL-STD-2217(AS): The following pages of MIL-STD-2217(AS) have been revised and supersede the pages listed.
MIL-STD-2217 (NOTICE 2)
MIL-STD-2217 (NOTICE 2), DEPARTMENT OF DEFENSE INTERFACE STANDARD: MEMORY LOADER/VERIFIER MULTIPLEX BUS INTERFACE WITH AVIONIC SYSTEMS, REQUIREMENTS FOR (22 MAY 2000)., TO ALL HOLDERS OF MIL-STD! -2217(AS): THE FOLLOWING PAGES OF MIL-STD-2217(AS) HAVE BEEN REVISED ANDSUPERSEDE THE PAGES LISTED:
MIL-STD-2217 (NOTICE 3)
MIL-STD-2217 (NOTICE 3), MILITARY STANDARD: MEMORY LOADER/VERIFIER MULTIPLEX BUS INTERFACE WITH AVIONICSYSTEMS, REQUIREMENTS FOR (22 FEB 2005)., MIL-STD-2217, dated 22 May 2000, has been reviewed and determinedto be valid for use in acquisition
MIL-STD-2218
MIL-STD-2218, MILITARY STANDARD: THERMAL DESIGN, ANALYSIS, AND TEST PROCEDURES FOR AIRBORNE ELECTRONIC EQUIPMENT (20 MAY 1992) [SUPERSEDING MIL-T-23103]., This standard establishes requirements for thermal design and cooling analyses, thermal design verification tests, and preproduction qualification tests for airborne electronic equipment. These thermal design requirements are provided to ensure that the equipment will operate satisfactorily without manual adju! stment under any mode of operation in the aircraft. It also es! tablishe s guidelines for test methods for verification testing of the thermal and cooling design and preproduction qualification temperature and humidity tests to ensure that the equipment meets its performance requirements and reliability criteria. This document defines a thermal design process establishing and validating the following: a. Equipment cooling methods and coolant flow requirements. b. Allowable component temperature and component power, based on derating requirements to achieve lowest component temperatures consistent with reliability and life cycle cost (LCC) requirements. c. A thermal design analysis which defines the temperatures, heat sources, heat paths and heat sinks of all temperature critical components for worst-case power, environmental temperature-altitude and coolant flow (where applicable) conditions. d. Thermal design, verification and preproduction qualification tests.
MIL-STD-2219A
M! IL-STD-2219A, DEPARTMENT OF DEFENSE STANDARD PRACTICE: FUSION WELDING FOR AEROSPACE APPLICATIONS (18 JUL 2005) [S/S by AWS-D17.1]., The scope of this document is to provide minimum requirements for weld filler materials, workmanship, inspection and record requirements for fusion welding of alloys applicable to aircraft, missiles, other aerospace equipment, their parts and accessories.
MIL-STD-2219A (w/CHANGE NOTICE 1)
MIL-STD-2219A (w/CHANGE NOTICE 1), DEPARTMENT OF DEFENSE STANDARD PRACTICE: FUSION WELDING FOR AEROSPACE APPLICATIONS (16 JUN 2008) [S/S BY AWS-D17.1]., The scope of this document is to provide minimum requirements for weld filler materials, workmanship, inspection and record requirements for fusion welding of alloys applicable to aircraft, missiles, other aerospace equipment, their parts and accessories.
MIL-STD-2219A (NOTICE 2)
MIL-STD-2219A (NOTICE 2), MILITARY STANDARD: FUSION WE! LDING FO R AEROSPACE APPLICATIONS (04 SEP 2009) [S/S BY AWS D17.1]., MIL-STD-2219A, dated 18 July 2005, is hereby canceled. Future acquisitions may refer to AWS D17.1, 揝pecification for Fusion Welding for Aerospace Applications.擴sers are cautioned to evaluate this document for their particular application before citing it as a replacement document.(Copies of AWS publications are available from www.aws.org or American Welding Society, 550 N.W. LeJeune Road, Miami FL 33126.)
MIL-STD-2219
MIL-STD-2219, MILITARY STANDARD: FUSION WELDING FOR AEROSPACE APPLICATIONS (30 DEC 1988) [SUPERSEDING MIL-W-8604A, MIL-W-8611A, & MIL-W-18326A] [S/S by AWS-D17.1]., The scope of this document is to provide minimum requirements for weld filler materials, workmanship, inspection and record requirements for fusion welding of alloys applicable to aircraft, missiles, other aerospace equipment, their parts and accessories.
MIL-STD-2219 (NOTICE 1)
MIL-STD-2219 (NOTICE 1), MILITARY STANDARD: FUSION WELDING FOR AEROSPACE APPLICATIONS (10 SEP 1999) [S/S by AWS-D17.1]., MIL-STD-2219, dated 30 December 1988, is hereby canceled. Future acquisition for this itemshould refer to SAE-AMS-STD-2219, "Fusion Welding for Aerospace Applications."(Application for copies of SAE Aerospace Material Specifications should be addressed to SAE,400 Commonwealth Drive, Warrendale, PA 15096-0001.)
MIL-STD-2219 (NOTICE 2)
MIL-STD-2219 (NOTICE 2), DEPARTMENT OF DEFENSE MILITARY STANDARD: FUSION WELDING FOR AEROSPACE APPLICATIONS (18 JUL 2005) [S/S by AWS-D17.1]., MIL-STD-2219, dated 30 December 1988, is hereby reinstated and may be used for acquisition.
MIL-STD-2220
MIL-STD-2220, DEPARTMENT OF DEFENSE INTERFAC! E STANDARD: SPECIFICATION FORMAT FOR TARGET AUXILIARY AND AUGM! ENTATION SYSTEMS (11 FEB 1988) [S/S BY MIL-STD-961]., This standard establishes the format, content, and procedures for the preparation of Target Auxiliary/Augmentation Systems (TA/AS) interface specifications.
MIL-STD-2220 (NOTICE 1)
MIL-STD-2220 (NOTICE 1), MILITARY STANDARD: SPECIFICATION FORMAT FOR TARGET AUXILIARY AND AUGMENTATION SYSTEMS (29 JAN 1996) [S/S BY MIL-STD-961]., MIL-STD-2220, dated 11 February 1988, is hereby canceled and superseded byMIL-STD-96HI, Standard Practice for Defense Specifications.
MIL-STD-2222 (NOTICE 1)
MIL-STD-2222 (NOTICE 1), MILITARY STANDARD: INTERFACE CONTROL DOCUMENTATION FOR AVIONICS SYSTEMS (29 SEP 1997) [S/S BY MIL-HDBK-2222]., MIL-STD-2222(AS) is hereby canceled. However the technical information and thelessons learned from this standard have been preserved in MIL-HDBK-2222(AS). MIL-HDBK-2222(AS) is for! guidance only and should not be cited as a requirement, the information in thehandbook may be useful in determining or evaluating requirements.
MIL-STD-2223
MIL-STD-2223, MILITARY STANDARD: TEST METHODS FOR INSULATED ELECTRIC WIRE (31 AUG 1992)., This standard establishes test methods for insulated wires made with tin-coated, silver-coated or nickel coated conductors of copper or copper alloy.
MIL-STD-2223 (NOTICE 1)
MIL-STD-2223 (NOTICE 1), MILITARY STANDARD: TEST METHODS FOR INSULATED ELECTRIC WIRE (09 SEP 1994)., TO ALL HOLDERS OF MIL-STD-2223: THE FOLLOWING METHODS ARE TO BE ADDED:
MIL-STD-2225
MIL-STD-2225, MILITARY STANDARD: VIBRATION AND NOISE TESTINGFOR INSTRUMENT BEARINGS (01 AUG 1994)., Vibration and noise measurements under controlled test conditions provi! de baseline data which can be used to ascertain relativebearin! g qualit y. The causes of vibration and noise are complex phenomena affected by many factors. This standard defines vibration and noise measurements under closely controlled conditions, and there is no guarantee that values measured in accordance with this standard will correlate with actual application.
MIL-STD-2301A
MIL-STD-2301A, DEPARTMENT OF DEFENSE: INTERFACE STANDARD COMPUTER GRAPHICS METAFILE (CGM) IMPLEMENTATION STANDARD FOR THE NATIONAL IMAGERY TRANSMISSION FORMAT STANDARD (05 JUN 1998) [NO S/S DOCUMENT]., This standard establishes the requirements necessary to implement Computer GraphicsMetafiles (CGMs) used for the representation of symbol graphics in the National Imagery Transmission FormatStandard (NITFS).
MIL-STD-2301A (NOTICE 1)
MIL-STD-2301A (NOTICE 1), DEPARTMENT OF DEFENSE INTERFACE STANDARD: COMPUTER GRAPHICS METAFILE (CGM) IM! PLEMENTATION STANDARD FOR THE NATIONAL IMAGERY TRANSMISSION FORMAT STANDARD (31 MAR 2004) [NO S/S DOCUMENT]., The purpose of this notice is to inform users of the change in name of the preparing activity fromthe National Imagery and Mapping Agency (NIMA) to the National Geospatial-IntelligenceAgency (NGA).
MIL-STD-2301A (NOTICE 2)
MIL-STD-2301A (NOTICE 2), DEPARTMENT OF DEFENSE INTERFACE STANDARD: COMPUTER GRAPHICS METAFILE (CGM) IMPLEMENTATION STANDARD FOR THE NATIONAL IMAGERY TRANSMISSION FORMAT STANDARD (22 MAR 2010) [NO S/S DOCUMENT]., MIL-STD-2301A, dated 5 June 1998, and any subsequent revisions or change notices are inactive for new design and shall be no longer used as a guidance reference for new designs.New designs should use International Standards Organization (ISO) Basic Imagery Interchange Format (BIIF) Profile for Computer Graphics Metafile Version 01.00. (BPCGM01.00) CAUTION: The superses! sion information is valid as of the date of
MIL-STD-2301
MIL-STD-2301, DEPARTMENT OF DEFENSE INTERFACE STANDARD: COMPUTER GRAPHICS METAFILE (CGM) IMPLEMENTATION STANDARD FOR THE NATIONAL IMAGERY TRANSMISSION FORMAT STANDARD (18 JUN 1993) [NO S/S DOCUMENT]., This standard establishes the requirements necessary to implement Computer Graphics Metafiles (CGM) used for the representation of symbol graphics in the National Imagery Transmission Format Standard (NITFS).
http://www.infoeach.com/item-10408.html
恭颂商祺 万事如意
---------------------------------------------------------------------
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MIL-STD-2217 (NOTICE 1), MILITARY STANDARD: MEMORY LOADER/VERIFIER MULTIPLEX BUS INTERFACE WITH AVIONIC SYSTEMS, REQUIREMENTS FOR (28 MAY 1993)., TO ALL HOLDERS OF MIL-STD-2217(AS): The following pages of MIL-STD-2217(AS) have been revised and supersede the pages listed.
MIL-STD-2217 (NOTICE 1)
MIL-STD-2217 (NOTICE 1), MILITARY STANDARD: MEMORY LOADER/VERIFIER MULTIPLEX BUS INTERFACE WITH AVIONIC SYSTEMS, REQUIREMENTS FOR (28 MAY 1993)., TO ALL HOLDERS OF MIL-STD-2217(AS): The following pages of MIL-STD-2217(AS) have been revised and supersede the pages listed.
MIL-STD-2217 (NOTICE 2)
MIL-STD-2217 (NOTICE 2), DEPARTMENT OF DEFENSE INTERFACE STANDARD: MEMORY LOADER/VERIFIER MULTIPLEX BUS INTERFACE WITH AVIONIC SYSTEMS, REQUIREMENTS FOR (22 MAY 2000)., TO ALL HOLDERS OF MIL-STD! -2217(AS): THE FOLLOWING PAGES OF MIL-STD-2217(AS) HAVE BEEN REVISED ANDSUPERSEDE THE PAGES LISTED:
MIL-STD-2217 (NOTICE 3)
MIL-STD-2217 (NOTICE 3), MILITARY STANDARD: MEMORY LOADER/VERIFIER MULTIPLEX BUS INTERFACE WITH AVIONICSYSTEMS, REQUIREMENTS FOR (22 FEB 2005)., MIL-STD-2217, dated 22 May 2000, has been reviewed and determinedto be valid for use in acquisition
MIL-STD-2218
MIL-STD-2218, MILITARY STANDARD: THERMAL DESIGN, ANALYSIS, AND TEST PROCEDURES FOR AIRBORNE ELECTRONIC EQUIPMENT (20 MAY 1992) [SUPERSEDING MIL-T-23103]., This standard establishes requirements for thermal design and cooling analyses, thermal design verification tests, and preproduction qualification tests for airborne electronic equipment. These thermal design requirements are provided to ensure that the equipment will operate satisfactorily without manual adju! stment under any mode of operation in the aircraft. It also es! tablishe s guidelines for test methods for verification testing of the thermal and cooling design and preproduction qualification temperature and humidity tests to ensure that the equipment meets its performance requirements and reliability criteria. This document defines a thermal design process establishing and validating the following: a. Equipment cooling methods and coolant flow requirements. b. Allowable component temperature and component power, based on derating requirements to achieve lowest component temperatures consistent with reliability and life cycle cost (LCC) requirements. c. A thermal design analysis which defines the temperatures, heat sources, heat paths and heat sinks of all temperature critical components for worst-case power, environmental temperature-altitude and coolant flow (where applicable) conditions. d. Thermal design, verification and preproduction qualification tests.
MIL-STD-2219A
M! IL-STD-2219A, DEPARTMENT OF DEFENSE STANDARD PRACTICE: FUSION WELDING FOR AEROSPACE APPLICATIONS (18 JUL 2005) [S/S by AWS-D17.1]., The scope of this document is to provide minimum requirements for weld filler materials, workmanship, inspection and record requirements for fusion welding of alloys applicable to aircraft, missiles, other aerospace equipment, their parts and accessories.
MIL-STD-2219A (w/CHANGE NOTICE 1)
MIL-STD-2219A (w/CHANGE NOTICE 1), DEPARTMENT OF DEFENSE STANDARD PRACTICE: FUSION WELDING FOR AEROSPACE APPLICATIONS (16 JUN 2008) [S/S BY AWS-D17.1]., The scope of this document is to provide minimum requirements for weld filler materials, workmanship, inspection and record requirements for fusion welding of alloys applicable to aircraft, missiles, other aerospace equipment, their parts and accessories.
MIL-STD-2219A (NOTICE 2)
MIL-STD-2219A (NOTICE 2), MILITARY STANDARD: FUSION WE! LDING FO R AEROSPACE APPLICATIONS (04 SEP 2009) [S/S BY AWS D17.1]., MIL-STD-2219A, dated 18 July 2005, is hereby canceled. Future acquisitions may refer to AWS D17.1, 揝pecification for Fusion Welding for Aerospace Applications.擴sers are cautioned to evaluate this document for their particular application before citing it as a replacement document.(Copies of AWS publications are available from www.aws.org or American Welding Society, 550 N.W. LeJeune Road, Miami FL 33126.)
MIL-STD-2219
MIL-STD-2219, MILITARY STANDARD: FUSION WELDING FOR AEROSPACE APPLICATIONS (30 DEC 1988) [SUPERSEDING MIL-W-8604A, MIL-W-8611A, & MIL-W-18326A] [S/S by AWS-D17.1]., The scope of this document is to provide minimum requirements for weld filler materials, workmanship, inspection and record requirements for fusion welding of alloys applicable to aircraft, missiles, other aerospace equipment, their parts and accessories.
MIL-STD-2219 (NOTICE 1)
MIL-STD-2219 (NOTICE 1), MILITARY STANDARD: FUSION WELDING FOR AEROSPACE APPLICATIONS (10 SEP 1999) [S/S by AWS-D17.1]., MIL-STD-2219, dated 30 December 1988, is hereby canceled. Future acquisition for this itemshould refer to SAE-AMS-STD-2219, "Fusion Welding for Aerospace Applications."(Application for copies of SAE Aerospace Material Specifications should be addressed to SAE,400 Commonwealth Drive, Warrendale, PA 15096-0001.)
MIL-STD-2219 (NOTICE 2)
MIL-STD-2219 (NOTICE 2), DEPARTMENT OF DEFENSE MILITARY STANDARD: FUSION WELDING FOR AEROSPACE APPLICATIONS (18 JUL 2005) [S/S by AWS-D17.1]., MIL-STD-2219, dated 30 December 1988, is hereby reinstated and may be used for acquisition.
MIL-STD-2220
MIL-STD-2220, DEPARTMENT OF DEFENSE INTERFAC! E STANDARD: SPECIFICATION FORMAT FOR TARGET AUXILIARY AND AUGM! ENTATION SYSTEMS (11 FEB 1988) [S/S BY MIL-STD-961]., This standard establishes the format, content, and procedures for the preparation of Target Auxiliary/Augmentation Systems (TA/AS) interface specifications.
MIL-STD-2220 (NOTICE 1)
MIL-STD-2220 (NOTICE 1), MILITARY STANDARD: SPECIFICATION FORMAT FOR TARGET AUXILIARY AND AUGMENTATION SYSTEMS (29 JAN 1996) [S/S BY MIL-STD-961]., MIL-STD-2220, dated 11 February 1988, is hereby canceled and superseded byMIL-STD-96HI, Standard Practice for Defense Specifications.
MIL-STD-2222 (NOTICE 1)
MIL-STD-2222 (NOTICE 1), MILITARY STANDARD: INTERFACE CONTROL DOCUMENTATION FOR AVIONICS SYSTEMS (29 SEP 1997) [S/S BY MIL-HDBK-2222]., MIL-STD-2222(AS) is hereby canceled. However the technical information and thelessons learned from this standard have been preserved in MIL-HDBK-2222(AS). MIL-HDBK-2222(AS) is for! guidance only and should not be cited as a requirement, the information in thehandbook may be useful in determining or evaluating requirements.
MIL-STD-2223
MIL-STD-2223, MILITARY STANDARD: TEST METHODS FOR INSULATED ELECTRIC WIRE (31 AUG 1992)., This standard establishes test methods for insulated wires made with tin-coated, silver-coated or nickel coated conductors of copper or copper alloy.
MIL-STD-2223 (NOTICE 1)
MIL-STD-2223 (NOTICE 1), MILITARY STANDARD: TEST METHODS FOR INSULATED ELECTRIC WIRE (09 SEP 1994)., TO ALL HOLDERS OF MIL-STD-2223: THE FOLLOWING METHODS ARE TO BE ADDED:
MIL-STD-2225
MIL-STD-2225, MILITARY STANDARD: VIBRATION AND NOISE TESTINGFOR INSTRUMENT BEARINGS (01 AUG 1994)., Vibration and noise measurements under controlled test conditions provi! de baseline data which can be used to ascertain relativebearin! g qualit y. The causes of vibration and noise are complex phenomena affected by many factors. This standard defines vibration and noise measurements under closely controlled conditions, and there is no guarantee that values measured in accordance with this standard will correlate with actual application.
MIL-STD-2301A
MIL-STD-2301A, DEPARTMENT OF DEFENSE: INTERFACE STANDARD COMPUTER GRAPHICS METAFILE (CGM) IMPLEMENTATION STANDARD FOR THE NATIONAL IMAGERY TRANSMISSION FORMAT STANDARD (05 JUN 1998) [NO S/S DOCUMENT]., This standard establishes the requirements necessary to implement Computer GraphicsMetafiles (CGMs) used for the representation of symbol graphics in the National Imagery Transmission FormatStandard (NITFS).
MIL-STD-2301A (NOTICE 1)
MIL-STD-2301A (NOTICE 1), DEPARTMENT OF DEFENSE INTERFACE STANDARD: COMPUTER GRAPHICS METAFILE (CGM) IM! PLEMENTATION STANDARD FOR THE NATIONAL IMAGERY TRANSMISSION FORMAT STANDARD (31 MAR 2004) [NO S/S DOCUMENT]., The purpose of this notice is to inform users of the change in name of the preparing activity fromthe National Imagery and Mapping Agency (NIMA) to the National Geospatial-IntelligenceAgency (NGA).
MIL-STD-2301A (NOTICE 2)
MIL-STD-2301A (NOTICE 2), DEPARTMENT OF DEFENSE INTERFACE STANDARD: COMPUTER GRAPHICS METAFILE (CGM) IMPLEMENTATION STANDARD FOR THE NATIONAL IMAGERY TRANSMISSION FORMAT STANDARD (22 MAR 2010) [NO S/S DOCUMENT]., MIL-STD-2301A, dated 5 June 1998, and any subsequent revisions or change notices are inactive for new design and shall be no longer used as a guidance reference for new designs.New designs should use International Standards Organization (ISO) Basic Imagery Interchange Format (BIIF) Profile for Computer Graphics Metafile Version 01.00. (BPCGM01.00) CAUTION: The superses! sion information is valid as of the date of
MIL-STD-2301
MIL-STD-2301, DEPARTMENT OF DEFENSE INTERFACE STANDARD: COMPUTER GRAPHICS METAFILE (CGM) IMPLEMENTATION STANDARD FOR THE NATIONAL IMAGERY TRANSMISSION FORMAT STANDARD (18 JUN 1993) [NO S/S DOCUMENT]., This standard establishes the requirements necessary to implement Computer Graphics Metafiles (CGM) used for the representation of symbol graphics in the National Imagery Transmission Format Standard (NITFS).
http://www.infoeach.com/item-10408.html
恭颂商祺 万事如意
---------------------------------------------------------------------
世界资料网提供各种行业资料， 国军标、 美军标、 美国汽车工程师协会 SAE、 美国材料测试协会 ASTM、 情报专利 期刊 、 会议论文、 统计数据、 海关资料数据 年鉴、 行业数据、 协会数据、 政府�! ��告、 商务部报告等。
网址:http://www.infoeach.com
Email: ke...@infoeach.com
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