MIL-STD-001591A COMMAND, CONTROL, AND COMMUNICATIONS SYSTEM AND COMPONENT (8 DEC 1978)., This standard establishes uniform criteria for conducting trade studies to determine the optimal design for command, control and communication system and component fault diagnosis/isolation subsystems.

MIL-STD-1500B (NOTICE 1), MILITARY STANDARD CADMIUM-TITANIUM PLATING, LOW EMBRITTLEMENT ELECTRO-DEPOSITION (9 DEC 1996)., MIL-STD-1500B, dated 2 April, 1990, 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.

MIL-STD-1500B, MILITARY STANDARD CADMIUM-TITANIUM PLATING, LOW EMBRITTLEMENT ELECTRO-DEPOSITION (2 APR 1990). This standard covers the process and materials required for the electro-deposition of cadmium-titanium on high strength steel substrates.

MIL-STD-1501B (NOTICE 1), MILITARY STANDARD CHROMIUM PLATING, LOW EMBRITTLEMENT, ELECTRODEPOSITION (14 DEC 1984)., The following pages of MIL-STD-1501B(USAF) have been revised and supersede the pages listed.

MIL-STD-1501B (USAF), MILITARY STANDARD CHROMIUM PLATING, LOW EMBRITTLEMENT, ELECTRODEPOSITION (29 MAR 1978)., This standard covers the process and materials required for the electrodeposition of chromium on high-strength steel substrates.

MIL-STD-1503B (NOTICE 1) MILITARY STANDARD PREPARATION OF ALUMINUM ALLOYS FOR SURFACE TREATMENTS AND INORGANIC COATING (2 AUG 1994)., MIL-STD-1503(USAF), dated 30 April 1973, has been reviewed and determined to be valid for use in acquisition.

MIL-STD-1503B (NOTICE 2) MILITARY STANDARD PREPARATION OF ALUMINUM ALLOYS FOR SURFACE TREATMENTS AND INORGANIC COATING (9 DEC 1996)., MIL-STD-1503B, dated 13 November, 1989, 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.

MIL-STD-1503B, MILITARY STANDARD PREPARATION OF ALUMINUM ALLOYS FOR SURFACE TREATMENTS AND INORGANIC COATING (13 NOV 1989)., This standard describes the cleaning, activation and underplating process, and material required for aluminum and aluminum alloys prior to applying inorganic coating. It is intended that this standard be used in conjunction with other process documents where the technical requirements are for the application of surface treatments and inorganic coatings on aluminum and aluminum alloys.

MIL-STD-1504B (NOTICE 1) MILITARY STANDARD ABRASIVE BLASTING. MIL-STD-1504B, dated 8 June, 1989, any any subsequent revisions or change notices are inactive for new design and shall be no longer used as a guidance reference for new designs.

MIL-STD-1504B, MILITARY STANDARD ABRASIVE BLASTING (8 JUN 1989)., This standard covers the processes and materials required for the abrasive blasting of aircraft and missile components.

MIL-STD-1510B (NOTICE 1) MILITARY STANDARD CONTAINER DESIGN RETRIEVAL SYSTEM PROCEDURES FOR USE OF. MIL-STD-1510B, dated 30 September 1988 is hereby cancelled. Future acquisitions should refer to MIL-STD-2073-1, Standard Practice for Military Packaging.

MIL-STD-1510B, MILITARY STANDARD CONTAINER DESIGN RETRIEVAL SYSTEM, PROCEDURES FOR USE OF. This standard provides DOD activities having packaging development/procurement responsibilities, and their contractors, the instructions for use of the Container Design Retrieval System (CDRD).

MIL-STD-1512 (USAF) (NOTICE 2), MILITARY STANDARD ELECTROEXPLOSIVE SUBSYSTEMS, ELECTRICALLY INITIATED, DESIGN REQUIREMENTS AND TEST METHODS. MILITARY STANDARD ELECTROEXPLOSIVE SUBSYSTEMS, ELECTRICALLY INITIATED, DESIGN REQUIREMENTS AND TEST METHODS MIL-STD-1512 (USAF), dated 21 March 1972 and Notice 1, dated 6 January 1976 are hereby canceled and superseded by MIL-HDBK-1512 (USAF), dated 30 September 1997.

MIL-STD-1512 (USAF), MILITARY STANDARD ELECTROEXPLOSIVE SUBSYSTEMS, ELECTRICALLY INITIATED, DESIGN RQMTS AND TEST METHODS. This standard establishes the general requirements and test methods for the design and development of electro-explosive subsystems and associated items to preclude hazards from unintentional initiation. These requirements apply to all subsystems utilizing electrically initiated, explosive, or pyrotechnic components.

MIL-STD-1514 (NOTICE 1) MILITARY STANDARD FITTINGS, TETRAFLOURETHLENE HOSE HIGH TEMPERATURE, HIGH PRESSURE (3000 psi) HYDRAULIC AND PNEMATIC CLASSIFICATION OF DEFECTS. MIL-STD-1514(USAF), dated 17 March 1971, has been reviewed and determined to be valid for use in acquisition.

MIL-STD-1514 (NOTICE 2) MILITARY STANDARD FITTINGS, TETRAFLOURETHLENE HOSE HIGH TEMPERATURE, HIGH PRESSURE (3000 PSI) HYDRAULIC AND PNEUMATIC CLASSIFICATION OF DEFECTS MIL-STD-1514, dated 17 March 1971, is hereby canceled without replacement.

MIL-STD-1514 (USAF), MILITARY STANDARD FITTINGS, TETRAFLUOROETHYLENE HOSE HIGH TEMPERATURE (3000 PSI) HYDRAULIC AND PNEUMATIC CLASSIFICATION OF DEFECTS. This standard covers the classification of defects for fittings covered by MIL-F-83296.

MIL-STD-1515A (NOTICE 1) MILITARY STANDARD FASTENER SYSTEMS FOR AEROSPACE APPLICATIONS (24 SEP 1979) [S/S BY NASM1515]., The following items of MIL-STD-1515A have been revised and supersede the items lised.

MIL-STD-1515A (NOTICE 2) FASTENER SYSTEMS FOR AEROSPACE APPLICATIONS (5 JUN 1981) [S/S BY NASM1515]., The following items of MIL-STD-1515A have been revised and supersede the items listed.

MIL-STD-1515A (NOTICE 3) MILITARY STANDARD, FASTENER SYSTEMS FOR AEROSPACE APPLICATIONS (24 JUN 1983) [S/S BY NASM1515]., The following items of MIL-STD-1515A have been revised and supersede the items listed.

MIL-STD-1515A (NOTICE 4) MILITARY STANDARD FASTENER SYSTEMS FOR AEROSPACE APPLICATIONS (4 MAY 1998) [S/S BY NASM1515]., MIL-STD-1515A, including Change Notice 3, dated 24 June 1983, is hereby canceled without replacement.

MIL-STD-1515A (NOTICE 5) MILITARY STANDARD FASTENER SYSTEMS FOR AEROSPACE APPLICATIONS (30 JUL 1999) [S/S BY NASM1515]., MIL-STD-1515, dated 4 May 1998, is hereby canceled. Future design should be done in accordance with NASM1515.

MIL-STD-1515A, MILITARY STANDARD FASTENER SYSTEMS FOR AEROSPACE APPLICATIONS (12 JUL 1978) [S/S BY NASM1515]., This standard covers the methods of fastening, materials, finishes, test methods, and hole size and criteria of fasteners and fastening systems used in the design and construction of aerospace systems. In addition, it provides a comprehensive presentation of approved engineering practices, procedures, processes, and characteristics for fasteners.

MIL-STD-1516A, MILITARY STANDARD UNIFIED CODE FOR COATINGS AND FINISHES FOR DOD MATERIEL. This standard is to establish a uniform code and to serve as a genera guide to the selection of suitable materials,procedures,and systems for cleaning,plating, painting and otherwise finishing metal, plastic,wood, and other surfaces,for use by the Department of Defense (DOD).

MIL-STD-1516B (NOTICE 1) MILITARY STANDARD UNIFIED CODE FOR COATINGS AND FINISHES FOR DOD MATERIAL. MIL-STD-1516B, dated 13 November 1990, is hereby canceled without replacement.

MIL-STD-1516B, MILITARY STANDARD UNIFIED CODE FOR COATINGS AND FINISHES FOR DOD MATERIAL. This standard establishes a uniform code and to serve as a general guide to the selection of suitable materials, procedures, and systems for cleaning, plating, painting, and otherwise finishing metal, plastic, wood, and other surfaces, for use by the Department of Defense (DOD).

MIL-STD-1518B (NOTICE 1) MILITARY STANDARD STORAGE, HANDLING, AND SERVICING OF AVIATION FUELS, LUBRICATING OILS, AND HYDRAULIC FLUIDS AT CONTRACTOR FACILITIES. This notice should be filed in front of MIL-STD-1518B, dated 3 March 1980. MIL-STD-15818B is Inactive for new design and is no longer used except for replacement purposes.

MIL-STD-1518B (NOTICE 2) STORAGE, HANDLING, AND SERVICING OF AVIATION FUELS, LUBRICATION OILS, AND HYDRAULIC FLUIDS AT CONTRACTOR LOCATIONS. MIL-STD-1518B, dated 3 March 1980, is hereby reactivated and may be used for new acquisition.

MIL-STD-1518B, MILITARY STANDARD STORAGE, HANDLING AND SERVICING OF AVIATION FUELS, LUBRICATING OILS AND HYDRAULIC FLUIDS AT CONTRACTOR FACILITIES. The purpose of this document is to set forth the performance requirements and quality control standards for receipt,storage, testing and servicing of all aviation fuels, lubricants and hydraulic fluids in support of USAF aircraft at manufacturing, maintenance or engine test facilities which are contractor operated.

MIL-STD-1518C, DEPARTMENT OF DEFENSE STANDARD PRACTICE STORAGE, HANDLING, AND SERVICING OF AVIATION FUELS, LUBRICATING OILS, AND HYDRAULIC FLUIDS AT CONTRACTOR FACILITIES. This standard establishes the minimum performance and quality requirements for the storage, handling, and servicing of aviation fuels, lubricating oils, and hydraulic fluids at contractor facilities.

MIL-STD-1519 (NOTICE 1) MILITARY STANDARD TEST REQUIREMENTS DOCUMENT. PREPARATION OF. To all holders of MIL-STD-1519 (USAF): 1. Pen and Ink Change: On self-cover change "Military Specification" to "Military Standard"

MIL-STD-1519 (NOTICE 2) MILITARY STANDARD TEST REQUIREMENTS DOCUMENT. PREPARATION OF MIL-STD-1519(USAF) dated September 1971 and Notice 1 dated 1 August 1977 have been reviewed and determined to be valid for use in acquisition

MIL-STD-1519 (NOTICE 3) MILITARY STANDARD TEST REQUIREMENTS DOCUMENT PREPARTION OF. MIL-STD-1519(usaf), dated 17 September 1971, NOTICE 1 of 1 August 1977, and NOTICE 2 of 26 February 1988 are hereby canceled without replacement.

MIL-STD-1519 (USAF), MILITARY SPECIFICATION TEST REQUIREMENTS DOCUMENTS, PREPARATION OF

MIL-STD-1520C (NOTICE 1), MILITARY STANDARD CORRECTIVE ACTION AND DISPOSITION SYSTEM FOR NONCONFORMING MATERIAL. The following pages of MIL-STD-1520C have been revised and supersede the pages listed.

MIL-STD-1520C (NOTICE 2), MILITARY STANDARD CORRECTIVE ACTION AND DISPOSITION SYSTEM FOR NONCONFORMING MATERIAL. MIL-STD-1520C, dated 27 June 1986, and Notice 1 dated 5 March 1993, are hereby canceled without replacement.

MIL-STD-1520C, MILITARY STANDARD CORRECTIVE ACTION AND DISPOSITION SYSTEM FOR NONCONFORMING MATERIAL. This standard sets forth the requirements for a cost-effective corrective action and disposition system for nonconforming material. It defines the requirements relative to the interface between the contractor and the contract administrative office on nonconforming material. This standard sets forth the DOD contracting activity requirements for a properly constituted Material Review Board (MRB).

MIL-STD-1521B (NOTICE 2) (USAF), MILITARY STANDARD TECHNICAL REVIEWS AND AUDITS FOR SYSTEMS, EQUIPMENTS, AND COMPUTER SOFTWARE (17 JUL 1992)., TO ALL HOLDERS OF MIL-STD-1521B (USAF) Pages 71 through 82, Appendix H, and Appendix I: DELETE. The contents of the pages listed are now contained in MIL-STD-973, “CONFIGURATION MANAGEMENT”.

MIL-STD-1521B (USAF) (NOTICE 3), MILITARY STANDARD TECHNICAL REVIEWS AND AUDITS FOR SYSTEMS, EQUIPMENTS, AND COMPUTER SOFTWARE (10 APR 1995)., MIL-STD-1521B (USAF), dated 4 June 1985, NOTICE 1 dated 19 December 1985, and NOTICE 2 dated 17 July 1992, are hereby canceled. Functional. Configuration Audit and physical Configuration Audit requirements were incorporated into MIL-STD-973, “Configuration Management.” All other areas have been canceled without replacement.

MIL-STD-1521B (USAF), MILITARY STANDARD TECHNICAL REVIEWS AND AUDITS FOR SYSTEMS, EQUIPMENTS, AND COMPUTER SOFTWARE (4 JUN 1985)., This standard prescribes the requirements for the conduct of Technical Reviews and Audits on Systems, Equipments, and Computer Software.

MIL-STD-1522A (NOTICE 1), MILITARY STANDARD STANDARD GENERAL REQUIREMENTS FOR SAFE DESIGN AND OPERATION OF PRESSURIZED MISSILE AND SPACE SYSTEMS (21 DEC 1984)., MIL-STD-1520C, dated 27 June 1986, and Notice 1 dated 21 December 1984, are hereby canceled without replacement.

MIL-STD-1522A (NOTICE 2), STANDARD GENERAL REQUIREMENTS FOR SAFE DESIGN AND OPERATION OF PRESSURIZED MISSILE AND SPACE SYSTEMS (20 NOV 1986)., The following pages of MIL-STD-1522A (USAF) have been revised and supersede the pages listed.

MIL-STD-1522A (NOTICE 3) STANDARD GENERAL REQUIREMENTS FOR SAFEDESIGN AND OPERATION OF PRESSURES MISSILE AND SPACE SYSTEMS MIL-STD-1522A (USAF), dated 28 May 84, has been reviewed and determined to be valid for use in acquisition.

MIL-STD-1522A (USAF), MILITARY STANDARD STANDARD GENERAL REQUIREMENTS FOR SAFE DESIGN AND OPERATION OF PRESSURIZED MISSILE AND SPACE SYSTEMS (28 MAY 1984)., This standard establishes requirements for the design and test of all pressurized systems for missiles, space vehicles and ground support equipment. These requirements, when implemented on a particular pressurized system, will assure a high level of confidence in achieving safe operation and mission success.

MIL-STD-1523A (NOTICE 1) AGE CONTROLS OF AGE-SENSITIVE ELASTOMERIC MATERIAL. MIL-STD-1523A. dated 1 February 1984, is hereby canceled. Future acquisitions should refer to SAE AS 1933. Age Controls for Hose Containing Age-Sensitive Elastomeric Material.

MIL-STD-1523A (NOTICE 2) AGE CONTROLS OF AGE-SENSITIVE ELASTOMERIC MATERIAL (FOR AEROSPACE APPLICATIONS) MIL-STD-1523A, dated 1 February 1984, is hereby canceled. Future acquisition for this product should refer to SAE-AS1933, "Age Control for Hose Containing Age-Sensitive ELastomeric Material" for hose application and SAE_ARP5316, "Storage of Aerospace Elastomeric Seals and Seal Assemblies which include an Elastomer Element prior to Hardware Assembly for seal application.

MIL-STD-1523A, MILITARY STANDARD AGE CONTROLS OF AGE-SENSITIVE ELASTOMERIC MATERIAL (FOR AEROSPACE APPLICATIONS). This document establishes requirements for the maximum ages of age sensitive elastomeric items for use in military aircraft and missiles and for space vehicles at the time of acceptance by a Government acquiring activity. The provisions of this document apply to hoses and O-r-s from specific classes of elastomers which are resistant to lubricants,hydraulic fluids,and petroleum base fuels and which conform to the specifications cited herein.

MIL-STD-1524 (NOTICE 1) TABLE OF DIFFERENTIAL PRESSURE IN RELATION TO CALIBRATED AIRSPEED The following pages of MIL-STD-1524 have been revised and supersede the pages listed

MIL-STD-1524 (NOTICE 2) TABLE OF DIFFERENTIAL PRESSURE IN RELATION TO CALIBRATED AIRSPEED. MIL-STD-1524. dated 31 July 1972, has been reviewed adn determined to be valid for use in acquisition.

MIL-STD-1524 (NOTICE 3) TABLE OF DIFFERENTIAL PRESSURE IN RELATION TO CALIBRATED AIRSPEED MIL-STD-1524 dated 31 July 1972, is hereby canceled without replacement.

MIL-STD-1524, MILITARY STANDARD TABLE OF DIFFERENTIAL PRESSURE IN RELATION TO CALIBRATED AIRSPEED. This standard presents differential pressures in inches of mercury and inches of water for values of calibrated airspeed in knots/

MIL-STD-1525B, DEPARTMENT OF DEFENSE STANDARD PRACTICE VERIFICATION TESTING OF PARACHUTE TEXTILE MATERIALS. This standard establishes the verification tests for parachute materials (subcontracted supplies) used in the fabrication of parachutes. These tests are for the purpose of confirming subcontractor test reports, determining conformance of material to contract specifications, and to provide data for the computation of reliability for these materials.

MIL-STD-1528A (NOTICE 1), MILITARY STANDARD MANUFACTURING MANAGEMENT PROGRAM. MIL-STD-1528A(USAF) , dated 9 September 1986, is hereby canceled without replacement.

MIL-STD-1528A, MILITARY STANDARD MANUFACTURING MANAGEMENT PROGRAM. The purpose of this standard is to prescribe the manufacturing management objectives and requirements which must be met by the contractor’s manufacturing management system on any contract which incorporates this standard. The system shall assure effective application of manufacturing management principles and methods to assure efficient manufacture, or preparation for manufacture, of defense acquisition programs hardware. The system shall establish, and assure application through program phases, crfterta for capability, capacity, producibility, productivity, manufacturing planning and risk reduction, strategic and critical materials conservation, and surge and mobilization to each aspect of hardware design, procurement, manufacture, and shipment.

MIL-STD-1529 (NOTICE 1) VENDOR SUBSTANTIATION FOR AEROSPACE PROPULSION SYSTEM ITEMS. Make the following pen and ink changes

MIL-STD-1529 (NOTICE 2) VENDOR SUBSTANATIATION FOR AEROSPACE PROPULSION SYSTEM ITEMS. MIL-STD-1529 dated 24 August 1972 and Notice 1 dated 28 February 1973, have been reviewed and determined to be valid for use in acquisition.

MIL-STD-1529 (NOTICE 3) VENDOR SUBSTANTABLE FOR AEROSPACE PROPULSION SYSTEM ITEMS MIL-STD-1529 dated 24 August 1972, is hereby canceled without replacement.

MIL-STD-1529 (USAF), MILITARY STANDARD VENDOR SUBSTANTIATION FOR AEROSPACE PROPULSION SYSTEM ITEMS. The purpose of this standard is to establish a requirement for and prescribe the procedure by which substantiation tests will be conducted for aerospace propulsion system items manufactured by fabrication sources not represented in the specific aerospace propulsion system which passed the aerospace propulsion system qualification tests.

MIL-STD-1530A (II), MILITARY STRUCTURAL INTEGRITY PROGRAM, AIRPLANE REQUIREMENTS. The purpose of this standard is to describe the Air Force Aircraft Structural Integrity Program, define the overall requirements necessary to achieve structural integrity of USAF airplanes, and specify acceptance methods of contractor compliance.

MIL-STD-1530A (USAF) (NOTICE 1), MILITARY STRUCTURAL INTEGRITY PROGRAM, AIRPLANE REQUIREMENTS. MIL-STD-1530A (USAF) dated 11 December 1975 has been reviewed and determined to be valid for use in acquisition.

MIL-STD-1530A (USAF) (NOTICE 2), MILITARY STRUCTURAL INTEGRITY PROGRAM, AIRPLANE REQUIREMENTS. MIL-STD-1530A, dated 26 February 1988, is hereby cancelled. Future acquisition should refer to MILHDBK- 1530, “Aircraft Structural Integrity Program, General Guidelines for.”

MIL-STD-1531 (USAF), MILITARY STANDARD INSERT ARRANGEMENTS FOR MIL-C-83733 RACK TO PANEL CONNECTORS, SHELL SIZE A. This standard covers insert arrangements for use with MIL-C-83733 panel to rack connectors, shell size A. It is used to control the dimensions and configuration of insert patterns and contact sizes.

MIL-STD-1531A (NOTICE 1) INSERT ARRANGEMENTS FOR MIL-C-83733 RACK TO PANEL CONNECTORS, SHRLL SIZE A. MIL-STD-1531A, dated 25 March 1988, has been reviewed and determined to be valid for use in acquisition.

MIL-STD-1531A, DEPARTMENT OF DEFENSE INTERFACE STANDARD INSERT ARRANGEMENTS FOR MIL-C-83733 RACK TO PANEL CONNECTORS, SHELL SIZE A. This standard covers insert arrangements for use with MIL-C_83733 rack to panel connectors, shell size A. It is used to control the dimensions and configuration of insert patterns and the contact sizes.

MIL-STD-1532, MILITARY STANDARD INSERT ARRANGEMENTS FOR MIL-C-83733 RACK TO PANEL CONNECTORS, SHELL SIZE B. This standard covers insert arrangements for use with MIL-C-83733 rack to panel connectors, shell size B. It is sued to control the dimensions and configuration of insert panels and the contact sizes.

MIL-STD-1532A (NOTICE 1) INSERT ARRANGEMENTS FOR MIL-C-83733 RACK TO PANEL CONNECTORS, SHRLL SIZE B. MIL-STD-1532A, dated 25 March 1988 has been reviewed and determined to be valid for use in acquisition.

MIL-STD-1532A, DEPARTMENT OF DEFENSE INTERFACE STANDARD INSERT ARRANGEMENTS FOR MIL-C-83733 RACK TO PANEL CONNECTORS, SHELL SIZE B. This standard covers insert arrangements for use with MIL-C-83733 rack to panel connectors, shell size B. It is used to control the dimensions and configuration of insert patterns and the contact sizes.

MIL-STD-1535, SUPPLIER QUALITY ASSURANCE PROGRAM REQUIREMENTS

MIL-STD-1535B, MILITARY STANDARD SUPPLIER QUALITY ASSURANCE PROGRAM REQUIREMENTS. The purpose of this standard is to establish contractor requirements and procedures for an effective quality assurance program for government acquisitions involving subcontracts when Higher-level Quality Assurance requirements, FAR 46.202-3, and this standard are requirements of the prime contract. The prim contractor shall tailor and include these requirements in purchase documents to suppliers.

MIL-STD-1537B (NOTICE 1) TEST METHOD STANDARD FOR ELECTRICAL CONDUCTIVITY TEST FOR VERIFICATION OF HEAT TREATMENT OF ALUMINUM ALLOYS EDDY CURRENT METHOD The following pages of MIL-STD_1537B have been revised and supersede the pages listed.

MIL-STD-1537B MILITARY STANDARD ELECTRICAL CONDUCTIVITY TEST FOR VERIFICATION OF HEAT TREATMENT OF ALUMINUM ALLOYS, EDDY CURRENT METHOD This standard contains procedures for verifying aluminum alloy heat treatment by means of eddy current techniques which measure electrical conductivity measurements are used in conjunction with hardness measurements.

MIL-STD-1537C, DEPARTMENT OF DEFENSE TEST METHOD STANDARD FOR ELECTRICAL CONDUCTIVITY TEST FOR VERIFICATION OF HEAT TREATMENT OF ALUMINUM ALLOYS EDDY CURRENT METHOD (25 JUN 2002)., This standard contains procedures for verifying aluminum alloy heat treatment by means of eddy current techniques, which measure electrical conductivity. Aluminum alloy heat treatment can be verified when electrical conductivity measurements are used in conjunction with hardness measurements.

MIL-STD-1538, MILITARY STANDARD, SPARE PARTS AND MAINTENANCE SUPPORT OF SPACE AND MISSILE SYSTEMS UNDERGOING RDT&E (11 APR 1973)., This standard establishes procedures under which the contractor shall provide spare parts and maintenance services.

MIL-STD-1539 (NOTICE 2), MILITARY STANDARD ELECTRICAL POWER, DIRECT CURRENT, SPACE VEHICLE DESIGN REQUIREMENTS. MIL-STD-1539, dated 4 September 1992, is inactive for new design and is no longer used, except for replacement purposes.

MIL-STD-1539 (USAF) (NOTICE 1), MILITARY STANDARD ELECTRICAL POWER, DIRECT CURRENT, SPACE VEHICLE DESIGN REQUIREMENTS. MIL-STD-1539 (USAF), dated 01 AUGUST 73, has been reviewed and determined to be valid for use in acquisition.

MIL-STD-1539 (USAF), MILITARY STANDARD ELECTRICAL POWER, DIRECT CURRENT, SPACE VEHICLE DESIGN REQUIREMENTS. This standard establishes the requirements for the direct current (DC) electrical power system for space vehicles.

MIL-STD-1540B (Notice 1) (USAF), MILITARY STANDARD TEST REQUIREMENTS FOR SPACE VEHICLES. Pages updated and superseded.

MIL-STD-1540B (Notice 2) (USAF), MILITARY STANDARD TEST REQUIREMENTS FOR SPACE VEHICLES. Pages updated and superseded.

This change notice incorporates special pyroshock screening tests for components that contain non-passivated microelectronic parts. THE FOLLOWING PAGES OF MIL-STD-1540B (USAF) HAVE BEEN REVISED AND SUPERSEDE THE PAGES LISTED:

MIL-STD-1540B, MILITARY STANDARD TEST REQUIREMENTS FOR SPACE VEHICLES. This standard establishes the environmental and structural ground testing requirements for launch vehicles, upper-stage vehicles, space vehicles, and for their subsystems and units.

MIL-STD-1540C, MILITARY STANDARD, TEST REQUIREMENTS FOR LAUNCH, UPPER-STAGE, AND SPACE VEHICLES (15 SEP 1994). This standard establishes the environmental and structural ground testing requirements for launch vehicles, upper-stage vehicles, space vehicles, and for their subsystems and units.

MIL-STD-1540D, PRODUCT VERIFICATION REQUIREMENTS FOR, LAUNCH, UPPER STAGE, AND SPACE VEHICLES. This standard establishes the environmental and structural ground testing requirements for launch vehicles, upper-stage vehicles, space vehicles, and for their subsystems and units.

MIL-STD-1541A, MILITARY STANDARD, ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS FOR SPACE SYSTEMS (30 DEC 1987)., This standard establishes the electromagnetic compatibility requirements for space systems, including frequency management, and the related requirements for the electrical and electronic equipment used in space systems. It also includes requirements designed to establish an effective ground reference for the installed equipment and designed to inhibit adverse electrostatic effects.

MIL-STD-1542A, MILITARY STANDARD ELECTROMAGNETIC COMPATIBILITY AND GROUNDING REQUIREMENTS FOR SPACE SYSTEM FACILITIES (1 MAY 1988)., The purpose of this standard is to specify the design, performance, and verification requirements for electrical subsystems for space system facilities, including electromagnetic compatibility (EMC), electrical power grounding, bonding, shielding, lightning protection, and TEMPEST security. These requirements are interrelated and interdependent, and therefore require an integrated approach in the design. .

MIL-STD-1542B (USAF), MILITARY STANDARD ELECTROMAGNETIC COMPATIBILITY AND GROUNDING REQUIREMENTS FOR SPACE SYSTEM FACILITIES (15 NOV 1991)., The purpose of this standard is to specify the design, performance, and verification requirements for electrical subsystems for space system facilities, including electromagnetic compatibility (EMC), electrical power grounding, bonding, shielding, lightning protection, and TEMPEST security. These requirements are interrelated and interdependent, and therefore require an integrated approach in the design. .

MIL-STD-1543B (NOTICE 1), MILITARY STANDARD, RELIABILITY PROGRAM REQUIREMENTS FOR SPACE AND LAUNCH VEHICLES (4 MAY 1998)., MIL-STD-1543B, dated 25 October 1988, is hereby canceled without replacement.

MIL-STD-1543B, MILITARY STANDARD, RELIABILITY PROGRAM REQUIREMENTS FOR SPACE AND LAUNCH VEHICLES (USAF) (25 OCT 1988)., This standard establishes uniform reliability program requirements and tasks for use during design, development, fabrication, test, and operation of space and launch vehicles.

MIL-STD-1545 (USAF) (NOTICE 1), OPTIONAL SPARE PARTS, MAINTENANCE AND INVENTORY SUPPORT OF SPACE AND MISSILE SYSTEMS (4 SEP 1992)., This standard establishes procedures under which the contractor will provide spare parts, inventory and maintenance services for space and missile systems.

MIL-STD-1545 (USAF), OPTIONAL SPARE PARTS, MAINTENANCE AND INVENTORY SUPPORT OF SPACE AND MISSILE SYSTEMS (15 JUN 1977)., This standard establishes procedures under which the contractor will provide spare parts, inventory and maintenance services for space and missile systems.

MIL-STD-1546B, MILITARY STANDARD, PARTS, MATERIALS, AND PROCESSES CONTROL PROGRAM FOR SPACE AND LAUNCH VEHICLES (27 JUL 1992)., This standard establishes the requirements for the preparation, implementation, and operation of a parts, materials, and processes control program for use during the design, development, and production of space and launch vehicles

MIL-STD-1547A, MILITARY STANDARD, ELECTRONIC PARTS, MATERIALS, AND PROCESSES FOR SPACE AND LAUNCH VEHICLES (1 DEC 1987) [S/S BY MIL-HDBK-1547]., This standard establishes the minimum technical requirements for parts, materials, and processes used in the design, development, and fabrication of space and launch vehicles.

MIL-STD-1547B, MILITARY STANDARD, ELECTRONIC PARTS, MATERIALS, AND PROCESSES FOR SPACE AND LAUNCH VEHICLES (1 DEC 1992) [S/S BY MIL-HDBK-1547]., This standard establishes the minimum technical requirements for parts, materials, and processes used in the design, development, and fabrication of space and launch vehicles.

MIL-STD-1548C (NOTICE 1) INTO-PLANE SERVICING OF FUELS AT COMMERCIAL AIRPORTS MIL-STD-1548C, dated 31 January 1994, is inactive for new design and is no longer used, except for replacement purposes.

MIL-STD-1548C (NOTICE 2) INTO-PLANE SERVICING OF FUELS AT COMMERCIAL AIRPORTS MIL-STD-1548C, dated 11 January 1994, is hereby reactivated and may be used for new acquisition.

MIL-STD-1548C MILITARY STANDARD INTO-PLANE SERVICING OF FUELS AT COMMERCIAL AIRPORTS This standard establishes the minimum performance and quality requirements for the servicing of fuels to aircraft on US Government Into-Plane Servicing Contracts at commercial airports.

MIL-STD-1548D, MILITARY STANDARD, INTO-PLANE SERVICING OF FUELS AT COMMERCIAL AIRPORTS (30 MAR 2000)., This standard establishes 2 types of standard practices for into-plane servicing of fuels at commercial airports.

MIL-STD-1548E, DEPARTMENT OF DEFENSE STANDARD PRACTICE INTO-PLANE SERVICING OF FUELS AT COMMERCIAL AIRPORTS. 1.1 This standard establishes two types of standard practices for into-plane servicing of fuels at commercial airports. Classification of into-plane servicing is as follows: Type I Into-Plane Refueling Guidance per ATA Specification 103, Standard For Jet Fuel Quality Control at Airports. Type II Into-Plane Refueling Guidance as per IATA's Guidelines for Aviation Fuel Quality Control and Operating Procedures for Joint Into-Plane Fueling Services (JIG).

MIL-ST