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MIL-HDBK (1500 - 1799)
MIL-HDBK-1512 (USAF), DOD HDBK ELECTROEXPLOSIVE SUBSYSTEMS, ELECTRICALLY INITIATED, DESIGN REQUIREMENTS AND TEST METHOD
MIL-HDBK-1512 (USAF), DOD HDBK ELECTRO-EXPLOSIVE SUBSYSTEMS, ELECTRICALLY INITIATED, DESIGN REQUIREMENTS AND TEST METHOD. This standard establishes the 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.
Ident. Num:
MIL-HDBK-1512
Rev. Num:
-
MIL-HDBK-1512 (USAF), DOD HDBK ELECTRO-EXPLOSIVE SUBSYSTEMS, ELECTRICALLY INITIATED, DESIGN REQUIREMENTS AND TEST METHOD. This standard establishes the 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-HDBK-1516 (NOTICE 1), MILITARY HANDBOOK UNIFIED CODE FOR COATINGS AND FINISHES FOR DOD MATERIAL
MIL-HDBK-1516 (NOTICE 1), MILITARY HANDBOOK UNIFIED CODE FOR COATINGS AND FINISHES FOR DOD MATERIAL. MIL-HDBK-1516, dated 24 January 1996, is hereby canceled without replacement.
Ident. Num:
MIL-HDBK-1516
MIL-HDBK-1516 (NOTICE 1), MILITARY HANDBOOK UNIFIED CODE FOR COATINGS AND FINISHES FOR DOD MATERIAL. MIL-HDBK-1516, dated 24 January 1996, is hereby canceled without replacement.
MIL-HDBK-1516, MILITARY HANDBOOK UNIFIED CODE FOR COATINGS AND FINISHES FOR DOD MATERIEL
MIL-HDBK-1516, MILITARY HANDBOOK UNIFIED CODE FOR COATINGS AND FINISHES FOR DOD MATERIEL. This handbook 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).
Ident. Num:
MIL-HDBK-1516
Rev. Num:
-
MIL-HDBK-1516, MILITARY HANDBOOK UNIFIED CODE FOR COATINGS AND FINISHES FOR DOD MATERIEL. This handbook 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-HDBK-1530 (USAF), MIL-HDBK-1530 (USA), DOD HDBK AIRCRAFT STRUCTURAL INTEGRITY PROGRAM, GENERAL GUIDELINES FOR
MIL-HDBK-1530 (USA), DOD HDBK AIRCRAFT STRUCTURAL INTEGRITY PROGRAM, GENERAL GUIDELINES FOR. 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. NOTE: Mil-Std-1530 has been re-designated as a Handbook, and is to be used for guidance purposes only. For administrative expediency, the only physical change from Mil-Std-1530 is this cover page. However, this document Is no longer to be cited as a requirement. If cited as a requirement, Contractors may disregard the requirement of this document and Interpret its contents only as guidance.
Ident. Num:
MIL-HDBK-1530
MIL-HDBK-1530 (USA), DOD HDBK AIRCRAFT STRUCTURAL INTEGRITY PROGRAM, GENERAL GUIDELINES FOR. 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. NOTE: Mil-Std-1530 has been re-designated as a Handbook, and is to be used for guidance purposes only. For administrative expediency, the only physical change from Mil-Std-1530 is this cover page. However, this document Is no longer to be cited as a requirement. If cited as a requirement, Contractors may disregard the requirement of this document and Interpret its contents only as guidance.
MIL-HDBK-1530A, DOD HANDBOOK AIRCRAFT STRUCTURAL INTEGRITY PROGRAM, GENERAL GUIDELINES FOR
MIL-HDBK-1530A, DOD HANDBOOK AIRCRAFT STRUCTURAL INTEGRITY PROGRAM, GENERAL GUIDELINES FOR. This handbook contains general guidelines for the U.S. Air Force Aircraft Structural Integrity Program (ASIP). These guidelines describe the processes proven successful in the achievement of structural integrity in USAF air vehicles while the cost of ownership is minimized; and cost and schedule risks managed through a series of disciplined, time-phased tasks. This handbook is for guidance only. This handbook cannot be cited as a requirement. If it is, the contractor does not have to comply.
Ident. Num:
MIL-HDBK-1530
Rev. Num:
A
MIL-HDBK-1530A, DOD HANDBOOK AIRCRAFT STRUCTURAL INTEGRITY PROGRAM, GENERAL GUIDELINES FOR. This handbook contains general guidelines for the U.S. Air Force Aircraft Structural Integrity Program (ASIP). These guidelines describe the processes proven successful in the achievement of structural integrity in USAF air vehicles while the cost of ownership is minimized; and cost and schedule risks managed through a series of disciplined, time-phased tasks. This handbook is for guidance only. This handbook cannot be cited as a requirement. If it is, the contractor does not have to comply.
MIL-HDBK-1530B (NOTICE 1), DEPARTMENT OF DEFENSE HANDBOOK AIRCRAFT STRUCTURAL INTEGRITY PROGRAM, GENERAL GUIDELINES FOR
MIL-HDBK-1530B (NOTICE 1), DEPARTMENT OF DEFENSE HANDBOOK AIRCRAFT STRUCTURAL INTEGRITY PROGRAM, GENERAL GUIDELINES FOR. MIL-HDBK-1530B(USAF), dated 3 July 2002, is hereby canceled and superseded by MIL-STD-1530B(USAF), “Aircraft Structural Integrity Program (ASIP).”
Ident. Num:
MIL-HDBK-1530
Rev. Num:
B
MIL-HDBK-1530B (NOTICE 1), DEPARTMENT OF DEFENSE HANDBOOK AIRCRAFT STRUCTURAL INTEGRITY PROGRAM, GENERAL GUIDELINES FOR. MIL-HDBK-1530B(USAF), dated 3 July 2002, is hereby canceled and superseded by MIL-STD-1530B(USAF), “Aircraft Structural Integrity Program (ASIP).”
MIL-HDBK-1530B, DOD HANDBOOK AIRCRAFT STRUCTURAL INTEGRITY PROGRAM, GENERAL GUIDELINES FOR
MIL-HDBK-1530B, DOD HANDBOOK AIRCRAFT STRUCTURAL INTEGRITY PROGRAM, GENERAL GUIDELINES FOR. This handbook contains general guidelines for the U.S. Air Force Aircraft Structural Integrity Program (ASIP). These guidelines describe the processes proven successful in the achievement of structural integrity in USAF air vehicles while the cost of ownership is minimized; and cost and schedule risks managed through a series of disciplined, time-phased tasks. This handbook is for guidance only. This handbook cannot be cited as a requirement. If it is, the contractor does not have to comply.
Ident. Num:
MIL-HDBK-1530
Rev. Num:
B
MIL-HDBK-1530B, DOD HANDBOOK AIRCRAFT STRUCTURAL INTEGRITY PROGRAM, GENERAL GUIDELINES FOR. This handbook contains general guidelines for the U.S. Air Force Aircraft Structural Integrity Program (ASIP). These guidelines describe the processes proven successful in the achievement of structural integrity in USAF air vehicles while the cost of ownership is minimized; and cost and schedule risks managed through a series of disciplined, time-phased tasks. This handbook is for guidance only. This handbook cannot be cited as a requirement. If it is, the contractor does not have to comply.
MIL-HDBK-1547, DOD HDBK ELECTRONIC PARTS, MATERIALS, AND PROCESSES FOR SPACE AND LAUNCH VEHICLES.
MIL-HDBK-1547, DOD HDBK ELECTRONIC PARTS, MATERIALS, AND PROCESSES FOR SPACE AND LAUNCH VEHICLES. This Handbook was developed to aid Designers and Parts, Materials, and Processes (PMP) specialists with the design, development, and fabrication of electronic systems required to have long life and/or high reliability while operating under extreme conditions/ environments of Space and Launch Vehicles. The purpose of this handbook is to establish and maintain consistent and uniform methods for development of technical requirements for electronic parts, materials, and processes used in the design, development, and fabrication of space and launch vehicles. It provides a common basis for estimating of Application Information, Design and Construction Considerations, and Quality Assurance Provisions for the proposed Design Application. It also establishes a common basis for comparing and evaluating of industry practices for related or competitive designs. This handbook is intended to be used as a tool to increase the performance and reliability of the system under design.
Ident. Num:
MIL-HDBK-1547
MIL-HDBK-1547, DOD HDBK ELECTRONIC PARTS, MATERIALS, AND PROCESSES FOR SPACE AND LAUNCH VEHICLES. This Handbook was developed to aid Designers and Parts, Materials, and Processes (PMP) specialists with the design, development, and fabrication of electronic systems required to have long life and/or high reliability while operating under extreme conditions/ environments of Space and Launch Vehicles. The purpose of this handbook is to establish and maintain consistent and uniform methods for development of technical requirements for electronic parts, materials, and processes used in the design, development, and fabrication of space and launch vehicles. It provides a common basis for estimating of Application Information, Design and Construction Considerations, and Quality Assurance Provisions for the proposed Design Application. It also establishes a common basis for comparing and evaluating of industry practices for related or competitive designs. This handbook is intended to be used as a tool to increase the performance and reliability of the system under design.
MIL-HDBK-1547A, DOD HDBK ELECTRONIC PARTS, MATERIALS, AND PROCESSES FOR SPACE AND LAUNCH VEHICLES
MIL-HDBK-1547A, DOD HDBK ELECTRONIC PARTS, MATERIALS, AND PROCESSES FOR SPACE AND LAUNCH VEHICLES. This Handbook was developed to aid Designers and Parts, Materials, and Processes (PMP) specialists with the design, development, and fabrication of electronic systems required to have long life and/or high reliability while operating under extreme conditions/ environments of Space and Launch Vehicles. The purpose of this handbook is to establish and maintain consistent and uniform methods for development of technical requirements for electronic parts, materials, and processes used in the design, development, and fabrication of space and launch vehicles. It provides a common basis for the estimation of Application Information, Design and Construction Considerations, and Quality Assurance Provisions for the proposed Design Application. It also establishes a common basis for comparing and evaluating of industry practices for related or competitive designs. This handbook is intended to be used as a tool to increase the performance and reliability of the system under design.
Ident. Num:
MIL-HDBK-1547
Rev. Num:
A
MIL-HDBK-1547A, DOD HDBK ELECTRONIC PARTS, MATERIALS, AND PROCESSES FOR SPACE AND LAUNCH VEHICLES. This Handbook was developed to aid Designers and Parts, Materials, and Processes (PMP) specialists with the design, development, and fabrication of electronic systems required to have long life and/or high reliability while operating under extreme conditions/ environments of Space and Launch Vehicles. The purpose of this handbook is to establish and maintain consistent and uniform methods for development of technical requirements for electronic parts, materials, and processes used in the design, development, and fabrication of space and launch vehicles. It provides a common basis for the estimation of Application Information, Design and Construction Considerations, and Quality Assurance Provisions for the proposed Design Application. It also establishes a common basis for comparing and evaluating of industry practices for related or competitive designs. This handbook is intended to be used as a tool to increase the performance and reliability of the system under design.
MIL-HDBK-1553A (NOTICE 3), MILITARY HANDBOOK MULTIPLEX APPLICATION HANDBOOK
MIL-HDBK-1553A (NOTICE 3), MILITARY HANDBOOK MULTIPLEX APPLICATION HANDBOOK. MIL-HDBK-1553A, dated 23 March 1995, has been reviewed and determined to be valid for use in acquisition
Ident. Num:
MIL-HDBK-1553
Rev. Num:
A
MIL-HDBK-1553A (NOTICE 3), MILITARY HANDBOOK MULTIPLEX APPLICATION HANDBOOK. MIL-HDBK-1553A, dated 23 March 1995, has been reviewed and determined to be valid for use in acquisition
MIL-HDBK-1553A (NOTICE 1), MILITARY HANDBOOK MULTIPLEX APPLICATIONS
MIL-HDBK-1553A (NOTICE 1), MILITARY HANDBOOK MULTIPLEX APPLICATIONS. MIL-HDBK-1553A, DATED 1 NOVEMBER 1988. HAS BEEN REVIEWED AND DETERMINED TO BE VALID FOR USE IN ACQUITION.
Ident. Num:
MIL-HDBK-1553
Rev. Num:
A
MIL-HDBK-1553A (NOTICE 1), MILITARY HANDBOOK MULTIPLEX APPLICATIONS. MIL-HDBK-1553A, DATED 1 NOVEMBER 1988. HAS BEEN REVIEWED AND DETERMINED TO BE VALID FOR USE IN ACQUITION.
MIL-HDBK-1553A (NOTICE 2), MILITARY HANDBOOK MULTIPLEX APPLICATIONS HANDBOOK
MIL-HDBK-1553A (NOTICE 2), MILITARY HANDBOOK MULTIPLEX APPLICATIONS HANDBOOK. The following changes should be made to MIL-HDBK-1553A, pages i and ii, "Delete Distribution Statement D and Export Control Warning Notice. Insert "Distribution Statement A - Approved for public release; distribution is unlimited."
Ident. Num:
MIL-HDBK-1553
Rev. Num:
A
MIL-HDBK-1553A (NOTICE 2), MILITARY HANDBOOK MULTIPLEX APPLICATIONS HANDBOOK. The following changes should be made to MIL-HDBK-1553A, pages i and ii, "Delete Distribution Statement D and Export Control Warning Notice. Insert "Distribution Statement A - Approved for public release; distribution is unlimited."
MIL-HDBK-1553A, MILITARY HANDBOOK MULTIPLEX APPLICATIONS HANDBOOK
This document provides rationale and guidance on the use of requirements contained in MIL-STD-1553B, Aircraft Internal Time Division Command/Response Multiplex Data Bus. New MlL-STD-1553 system designs and advances in microelectronics since the first MIL-HDBK-1553 was published were the motivation for this revision. It describes new MlL-STD-1553 state-of-the-art multiplexing, it retains the valuable fundamentals of the original handbook, and it contains help for— a. Government engineers who write requirements for equipment with MlL-STD-1553 interfaces or specify systems that conform to MlL-STD-1553. “Black box” designers who design equipment that interfaces with the MlL-STD-1553 multiplex bus. System designers and integrators who design systems incorporating multiple units that communicate via a MlL-STD-1553 multiplex bus.
Ident. Num:
MIL-HDBK-1553
Rev. Num:
A
This document provides rationale and guidance on the use of requirements contained in MIL-STD-1553B, Aircraft Internal Time Division Command/Response Multiplex Data Bus. New MlL-STD-1553 system designs and advances in microelectronics since the first MIL-HDBK-1553 was published were the motivation for this revision. It describes new MlL-STD-1553 state-of-the-art multiplexing, it retains the valuable fundamentals of the original handbook, and it contains help for— a. Government engineers who write requirements for equipment with MlL-STD-1553 interfaces or specify systems that conform to MlL-STD-1553. “Black box” designers who design equipment that interfaces with the MlL-STD-1553 multiplex bus. System designers and integrators who design systems incorporating multiple units that communicate via a MlL-STD-1553 multiplex bus.
MIL-HDBK-1559, DOD HDBK, NUMBERS, SERIAL, AIRCRAFT GAS TURBINE ENGINE AND ENGINE MODULE ASSIGNMENT OF
MIL-HDBK-1559, DOD HDBK, NUMBERS, SERIAL, AIRCRAFT GAS TURBINE ENGINE AND ENGINE MODULE ASSIGNMENT OF. This standard describes the method of assignment and arrangement of letters and numerals used by the Military Services to identify complete engines and modules (major sub-assemblies thereof) as to the manufacturer and series in production.
Ident. Num:
MIL-HDBK-1559
Rev. Num:
A
MIL-HDBK-1559, DOD HDBK, NUMBERS, SERIAL, AIRCRAFT GAS TURBINE ENGINE AND ENGINE MODULE ASSIGNMENT OF. This standard describes the method of assignment and arrangement of letters and numerals used by the Military Services to identify complete engines and modules (major sub-assemblies thereof) as to the manufacturer and series in production.
MIL-HDBK-1559A (NOTICE 1), DOD HDBK, NUMBERS, SERIAL, AIRCRAFT GAS TURBINE ENGINE AND ENGINE MODULE ASSIGNMENT OF
MIL-HDBK-1559 (NOTICE 1), DOD HDBK, NUMBERS, SERIAL, AIRCRAFT GAS TURBINE ENGINE AND ENGINE MODULE ASSIGNMENT OF. MIL-STD-1559, dated 1 January 1984, has been reviewed and determined to be valid for use in acquisition.
Ident. Num:
MIL-HDBK-1559
Rev. Num:
A
MIL-HDBK-1559 (NOTICE 1), DOD HDBK, NUMBERS, SERIAL, AIRCRAFT GAS TURBINE ENGINE AND ENGINE MODULE ASSIGNMENT OF. MIL-STD-1559, dated 1 January 1984, has been reviewed and determined to be valid for use in acquisition.
MIL-HDBK-1559A (NOTICE 2), DOD HDBK, NUMBERS, SERIAL, AIRCRAFT GAS TURBINE ENGINE AND ENGINE MODULE ASSIGNMENT OF
MIL-HDBK-1559A (NOTICE 2), DOD HDBK, NUMBERS, SERIAL, AIRCRAFT GAS TURBINE ENGINE AND ENGINE MODULE ASSIGNMENT OF. The following changes form a part of MIL-STD-1559A, dated 1 January 1984, and is approved for use by all departments and agencies of the Department of Defense.
Ident. Num:
MIL-HDBK-1559
Rev. Num:
A
MIL-HDBK-1559A (NOTICE 2), DOD HDBK, NUMBERS, SERIAL, AIRCRAFT GAS TURBINE ENGINE AND ENGINE MODULE ASSIGNMENT OF. The following changes form a part of MIL-STD-1559A, dated 1 January 1984, and is approved for use by all departments and agencies of the Department of Defense.
MIL-HDBK-1568 (USAF), MILITARY HANDBOOK MATERIALS AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN AEROSPACE WEAPONS SYSTEMS (18 JUL 1996)
MIL-HDBK-1568 (USAF), MILITARY HANDBOOK MATERIALS AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN AEROSPACE WEAPONS SYSTEMS (18 JUL 1996). This standard establishes the requirements for materials, processes and techniques, and identifies the tasks required to implement an effective corrosion prevention and control program during the conceptual, validation, development and production phases of aerospace weapon systems. The intent is to minimize life cycle cost due to corrosion and to obtain improved reliability.
Ident. Num:
MIL-HDBK-1568
Rev. Num:
-
MIL-HDBK-1568 (USAF), MILITARY HANDBOOK MATERIALS AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN AEROSPACE WEAPONS SYSTEMS (18 JUL 1996). This standard establishes the requirements for materials, processes and techniques, and identifies the tasks required to implement an effective corrosion prevention and control program during the conceptual, validation, development and production phases of aerospace weapon systems. The intent is to minimize life cycle cost due to corrosion and to obtain improved reliability.
MIL-HDBK-1587, DEPARTMENT OF DEFENSE HANDBOOK MATERIALS AND PROCESS REQUIREMENTS FOR AIR FORCE WEAPON SYSTEMS (18 JUL 1996)
MIL-HDBK-1587, DEPARTMENT OF DEFENSE HANDBOOK MATERIALS AND PROCESS REQUIREMENTS FOR AIR FORCE WEAPON SYSTEMS (18 JUL 1996). This standard establishes the requirements for materials and processes used during design and production of aerospace weapon systems. When used in conjunction with MIL-STD-1 530, the other integrity~ program documents (MIL-STD-1783, 1798, etc.), and MIL-STD-1568, it is expected that structurally reliable aerospace systems having a good balance between acquisition costs and life cycle costs will result.
Ident. Num:
MIL-HDBK-1587
Rev. Num:
-
MIL-HDBK-1587, DEPARTMENT OF DEFENSE HANDBOOK MATERIALS AND PROCESS REQUIREMENTS FOR AIR FORCE WEAPON SYSTEMS (18 JUL 1996). This standard establishes the requirements for materials and processes used during design and production of aerospace weapon systems. When used in conjunction with MIL-STD-1 530, the other integrity~ program documents (MIL-STD-1783, 1798, etc.), and MIL-STD-1568, it is expected that structurally reliable aerospace systems having a good balance between acquisition costs and life cycle costs will result.
MIL-HDBK-1599A (NOTICE 2),Bearings, Control System Components, and Associated Hardware used in the Design/Construction of Aerospace Mechanical Systems
MIL-HDBK-1599A (NOTICE 2),Bearings, Control System Components, and Associated Hardware used in the Design/Construction of Aerospace Mechanical Systems. THE FOLLOWING PAGES OF MIL-HDBK-1599A, SECTION 100 IS MISSING AND NEEDS TO BE INSERTED:
Ident. Num:
MIL-HDBK-1599
Rev. Num:
A
MIL-HDBK-1599A (NOTICE 2),Bearings, Control System Components, and Associated Hardware used in the Design/Construction of Aerospace Mechanical Systems. THE FOLLOWING PAGES OF MIL-HDBK-1599A, SECTION 100 IS MISSING AND NEEDS TO BE INSERTED:
MIL-HDBK-1599A (NOTICE 2),Bearings, Control System Components, and Associated Hardware used in the Design/Construction of Aerospace Mechanical Systems
MIL-HDBK-1599A (NOTICE 2),Bearings, Control System Components, and Associated Hardware used in the Design/Construction of Aerospace Mechanical Systems. 1. THE FOLLOWING PAGE OF MIL-HDBK-1599A, SECTION 601-6 IS INCORRECT AND NEEDS TO BE DELETED: 3.5.1.1 Material and configuration. The material, configuration, and quality shall conform to MIL-T-8878 and MS21251. Steel turnbuckles are not approved for aircraft use. 3.5.1.2 Usage. The MS21251 aluminum and brass turnbuckles are approved for primary controls, secondary controls, and auxiliary cable assemblies. The appropriate size turnbuckle shall be used for the applicable size cable as noted on MS21251. 3.5.1.3 Strength. The MS21251 aluminum and brass turnbuckles shall withstand the minimum breaking strength of the appropriate size cable. Size selection shall be on this basis. 2. Presently this document contains a requirement that prohibits the use of steel turnbuckles on aircraft. Recently a galling/chip problem with brass turnbuckles used on aircraft was reported. This problem was resolved by using steel turnbuckle bodies as specified in MIL-DTL-8878, a specification developed exclusively for aircraft control applications. Furthermore, MS21251, which serves as the basic MIL-HDBK-1599 aircraft turnbuckle standard, includes the use of steel materials. Research into this issue indicates that the reason for establishing this part of Requirement 601, paragraph 3.5.1.1 was a corrosion problem with the steel bodies. However, the current specification governing these parts requires the use of cadmium plating on these parts eliminating the corrosion problems that may have existed back when this requirement was generated. An administrative change was the best thing to use to correct this Mil Handbook and a revision is being planned.
Ident. Num:
MIL-HDBK-1599
Rev. Num:
A
MIL-HDBK-1599A (NOTICE 2),Bearings, Control System Components, and Associated Hardware used in the Design/Construction of Aerospace Mechanical Systems. 1. THE FOLLOWING PAGE OF MIL-HDBK-1599A, SECTION 601-6 IS INCORRECT AND NEEDS TO BE DELETED: 3.5.1.1 Material and configuration. The material, configuration, and quality shall conform to MIL-T-8878 and MS21251. Steel turnbuckles are not approved for aircraft use. 3.5.1.2 Usage. The MS21251 aluminum and brass turnbuckles are approved for primary controls, secondary controls, and auxiliary cable assemblies. The appropriate size turnbuckle shall be used for the applicable size cable as noted on MS21251. 3.5.1.3 Strength. The MS21251 aluminum and brass turnbuckles shall withstand the minimum breaking strength of the appropriate size cable. Size selection shall be on this basis. 2. Presently this document contains a requirement that prohibits the use of steel turnbuckles on aircraft. Recently a galling/chip problem with brass turnbuckles used on aircraft was reported. This problem was resolved by using steel turnbuckle bodies as specified in MIL-DTL-8878, a specification developed exclusively for aircraft control applications. Furthermore, MS21251, which serves as the basic MIL-HDBK-1599 aircraft turnbuckle standard, includes the use of steel materials. Research into this issue indicates that the reason for establishing this part of Requirement 601, paragraph 3.5.1.1 was a corrosion problem with the steel bodies. However, the current specification governing these parts requires the use of cadmium plating on these parts eliminating the corrosion problems that may have existed back when this requirement was generated. An administrative change was the best thing to use to correct this Mil Handbook and a revision is being planned.
MIL-HDBK-1599A,, Bearings, Control System Components, and Associated Hardware used in the Design and Construction of Aerospace Mechanical Systems
MIL-HDBK-1599A, Bearings, Control System Components, and Associated Hardware used in the Design and Construction of Aerospace Mechanical Systems and Subsystems. This handbook is intended to assist engineers in the design and construction of aerospace mechanical systems for military aircraft. It is intended to serve the engineer by fostering the use of approved standards parts while allowing the freedom to choose non-standard or special parts when a particular application warrants it. It is intended to neither tie the designer's hands nor to grant unlimited license. This handbook is intended to assist engineers: (a) by providing design guidance based on industry-proven engineering practices for bearings, control system components and associated hardware used in aerospace mechanical systems; (b) by requiring the use of approved standard parts in these systems to the largest extent practicable; and (c) by providing for the selection and approval of special parts, when those are necessary and appropriate, through the use of defined procedures.
Ident. Num:
MIL-HDBK-1599
Rev. Num:
A
MIL-HDBK-1599A, Bearings, Control System Components, and Associated Hardware used in the Design and Construction of Aerospace Mechanical Systems and Subsystems. This handbook is intended to assist engineers in the design and construction of aerospace mechanical systems for military aircraft. It is intended to serve the engineer by fostering the use of approved standards parts while allowing the freedom to choose non-standard or special parts when a particular application warrants it. It is intended to neither tie the designer's hands nor to grant unlimited license. This handbook is intended to assist engineers: (a) by providing design guidance based on industry-proven engineering practices for bearings, control system components and associated hardware used in aerospace mechanical systems; (b) by requiring the use of approved standard parts in these systems to the largest extent practicable; and (c) by providing for the selection and approval of special parts, when those are necessary and appropriate, through the use of defined procedures.
MIL-HDBK-1655, DEPARTMENT OF DEFENSE HANDBOOK CLASSIFICATION OF DEFECTS OF FLARELESS AND BEAM SEAL FITTINGS
MIL-HDBK-1655, DEPARTMENT OF DEFENSE HANDBOOK CLASSIFICATION OF DEFECTS OF FLARELESS AND BEAM SEAL FITTINGS. This handbook establishes a classification of commonly occurring defects applicable to flareless fittings and beam seal fittings specified in military specifications MIL-F-18280, MIL-F-85421, MIL-F-85720, and DoD adopted non-Government standards.
Ident. Num:
MIL-HDBK-1655
Rev. Num:
-
MIL-HDBK-1655, DEPARTMENT OF DEFENSE HANDBOOK CLASSIFICATION OF DEFECTS OF FLARELESS AND BEAM SEAL FITTINGS. This handbook establishes a classification of commonly occurring defects applicable to flareless fittings and beam seal fittings specified in military specifications MIL-F-18280, MIL-F-85421, MIL-F-85720, and DoD adopted non-Government standards.
MIL-HDBK-1670, DEPARTMENT OF DEFENSE HANDBOOK ENVIRONMENTAL CRITERIA AND GUIDELINES FOR AIR-LAUNCHED WEAPONS (7 DEC 2007) [SUPERSEDING MIL-STD-1670]
MIL-HDBK-1670, DEPARTMENT OF DEFENSE HANDBOOK ENVIRONMENTAL CRITERIA AND GUIDELINES FOR AIR-LAUNCHED WEAPONS (7 DEC 2007) [SUPERSEDING MIL-STD-1670]., This handbook establishes guidelines for the development of environmental engineering design and test requirements for air-launched weapons.
Ident. Num:
MIL-HDBK-1670
Rev. Num:
-
MIL-HDBK-1670, DEPARTMENT OF DEFENSE HANDBOOK ENVIRONMENTAL CRITERIA AND GUIDELINES FOR AIR-LAUNCHED WEAPONS (7 DEC 2007) [SUPERSEDING MIL-STD-1670]., This handbook establishes guidelines for the development of environmental engineering design and test requirements for air-launched weapons.
MIL-HDBK-1760, MILITARY HANDBOOK AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM
MIL-HDBK-1760, MILITARY HANDBOOK AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM. This Handbook was developed by a team including members from the three US military services, the UK MOD, the SAE AS-1B committee, and contractors. It includes information previously published in document ASD-TR-87-5028 with certain elements of ASD-TR-91-5009. Some of this information was also published in DEF-STAN-00-69 (Part II), which is written around MIL-STD-1760B. This version of this Handbook is written around MIL-STD-1760C and assumes that the reader is also reading 1760C. 2. This Handbook provides information on the implementation of a standardized electrical interconnection system, as defined by MIL-STD-1760, into both current and future aircraft and stores. It provides guidance on design considerations and options for including the standard interface capability at the aircraft's store stations and for providing a common electrical interface on carriage stores and mission stores. As a handbook, it cannot be invoked as a requirement in a contract. 3. Trends in weapon system designs (aircraft and stores) caused concern over the general proliferation of aircraft-to-store electrical interfacing requirements and the resulting high cost to achieve interoperability between aircraft and stores. The intent of MIL-STD-1760 is to reduce the aircraft/store electrical integration problem by specifying a standard electrical interface between aircraft and stores. The standard electrical interface is based on recognized trends in store management systems which use serial digital data transmission for control, monitor and release of stores.
Ident. Num:
MIL-HDBK-1760
Rev. Num:
-
MIL-HDBK-1760, MILITARY HANDBOOK AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM. This Handbook was developed by a team including members from the three US military services, the UK MOD, the SAE AS-1B committee, and contractors. It includes information previously published in document ASD-TR-87-5028 with certain elements of ASD-TR-91-5009. Some of this information was also published in DEF-STAN-00-69 (Part II), which is written around MIL-STD-1760B. This version of this Handbook is written around MIL-STD-1760C and assumes that the reader is also reading 1760C. 2. This Handbook provides information on the implementation of a standardized electrical interconnection system, as defined by MIL-STD-1760, into both current and future aircraft and stores. It provides guidance on design considerations and options for including the standard interface capability at the aircraft's store stations and for providing a common electrical interface on carriage stores and mission stores. As a handbook, it cannot be invoked as a requirement in a contract. 3. Trends in weapon system designs (aircraft and stores) caused concern over the general proliferation of aircraft-to-store electrical interfacing requirements and the resulting high cost to achieve interoperability between aircraft and stores. The intent of MIL-STD-1760 is to reduce the aircraft/store electrical integration problem by specifying a standard electrical interface between aircraft and stores. The standard electrical interface is based on recognized trends in store management systems which use serial digital data transmission for control, monitor and release of stores.
MIL-HDBK-1763, AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES
MIL-HDBK-1763, AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES. This handbook applies to all agencies within the DoD and industry involved with determining the extent of compatibility between military aircraft and aircraft stores. It applies to every activity of the system life cycle involving aircraft and/or stores including: development, manufacturing, deployment, operations, support, training and disposal. This handbook is for guidance only. This handbook cannot be cited as a requirement. If it is, the contractor does not have to comply.
Ident. Num:
MIL-HDBK-1763
Rev. Num:
-
MIL-HDBK-1763, AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES. This handbook applies to all agencies within the DoD and industry involved with determining the extent of compatibility between military aircraft and aircraft stores. It applies to every activity of the system life cycle involving aircraft and/or stores including: development, manufacturing, deployment, operations, support, training and disposal. This handbook is for guidance only. This handbook cannot be cited as a requirement. If it is, the contractor does not have to comply.
MIL-HDBK-1783A, DEPARTMENT OF DEFENSE HANDBOOK ENGINE STRUCTURAL INTEGRITY PROGRAM (ENSIP)
MIL-HDBK-1783A, DEPARTMENT OF DEFENSE HANDBOOK ENGINE STRUCTURAL INTEGRITY PROGRAM (ENSIP). This handbook establishes structural performance, design development, and verification guidance for turbine engines. This handbook also establishes the need for an Engine Structural Integrity Program (ENSIP). This handbook is for guidance only. This handbook cannot be cited as a requirement. If it is, the contractor does not have to comply.
Ident. Num:
MIL-HDBK-1783
Rev. Num:
A
MIL-HDBK-1783A, DEPARTMENT OF DEFENSE HANDBOOK ENGINE STRUCTURAL INTEGRITY PROGRAM (ENSIP). This handbook establishes structural performance, design development, and verification guidance for turbine engines. This handbook also establishes the need for an Engine Structural Integrity Program (ENSIP). This handbook is for guidance only. This handbook cannot be cited as a requirement. If it is, the contractor does not have to comply.
MIL-HDBK-1783B (NOTICE 1), DEPARTMENT OF DEFENSE HANDBOOK ENGINE STRUCTURAL INTEGRITY PROGRAM (ENSIP)
MIL-HDBK-1783B (NOTICE 1), DEPARTMENT OF DEFENSE HANDBOOK ENGINE STRUCTURAL INTEGRITY PROGRAM (ENSIP). THE FOLLOWING PAGES OF MIL-HDBK-1783B HAVE BEEN REVISED AND SUPERSEDE THE PAGES LISTED:
Ident. Num:
MIL-HDBK-1783
Rev. Num:
B
MIL-HDBK-1783B (NOTICE 1), DEPARTMENT OF DEFENSE HANDBOOK ENGINE STRUCTURAL INTEGRITY PROGRAM (ENSIP). THE FOLLOWING PAGES OF MIL-HDBK-1783B HAVE BEEN REVISED AND SUPERSEDE THE PAGES LISTED:
MIL-HDBK-1783B, DEPARTMENT OF DEFENSE HANDBOOK ENGINE STRUCTURAL INTEGRITY PROGRAM (ENSIP)
MIL-HDBK-1783B, DEPARTMENT OF DEFENSE HANDBOOK ENGINE STRUCTURAL INTEGRITY PROGRAM (ENSIP).The purpose of this handbook is to establish structural performance, design development, and verification guidance to ensure structural integrity for engine systems. The guidance contained herein includes the experience and lessons learned achieved during development of U.S. Air Force engine systems since the mid-1940s. Recent experience indicates superior structural safety and durability, including minimum structural maintenance, can be achieved on an engine system if the guidance contained herein is included and successfully executed during system development. This handbook is intended for use in conjunction with JSSG-2007, Aircraft Turbine Engines, on engine development programs or by itself when used for commercial (off-the-shelf) acquisitions.
Ident. Num:
MIL-HDBK-1783
Rev. Num:
B
MIL-HDBK-1783B, DEPARTMENT OF DEFENSE HANDBOOK ENGINE STRUCTURAL INTEGRITY PROGRAM (ENSIP).The purpose of this handbook is to establish structural performance, design development, and verification guidance to ensure structural integrity for engine systems. The guidance contained herein includes the experience and lessons learned achieved during development of U.S. Air Force engine systems since the mid-1940s. Recent experience indicates superior structural safety and durability, including minimum structural maintenance, can be achieved on an engine system if the guidance contained herein is included and successfully executed during system development. This handbook is intended for use in conjunction with JSSG-2007, Aircraft Turbine Engines, on engine development programs or by itself when used for commercial (off-the-shelf) acquisitions.
MIL-HDBK-1785, SYSTEM SECURITY ENGINEERING PROGRAM MANAGEMENT REQUIREMENTS
MIL-HDBK-1785, SYSTEM SECURITY ENGINEERING PROGRAM MANAGEMENT REQUIREMENTS. This standard establishes the formats, contents and procedures for a contract SSE Management Program. The purpose of the system Security Engineering Management Program is to establish definitive guidance in the initial acquisition or modification of new or existing systems, equipment, and facilities to analyze security design and engineering vulnerabilities; and develop recommendations for engineering changes to eliminate or mitigate vulnerabilities consistent with other design and operational considerations. SSE supports the development of programs and standards to provide life cycle security for critical defense resources.
Ident. Num:
MIL-HDBK-1785
MIL-HDBK-1785, SYSTEM SECURITY ENGINEERING PROGRAM MANAGEMENT REQUIREMENTS. This standard establishes the formats, contents and procedures for a contract SSE Management Program. The purpose of the system Security Engineering Management Program is to establish definitive guidance in the initial acquisition or modification of new or existing systems, equipment, and facilities to analyze security design and engineering vulnerabilities; and develop recommendations for engineering changes to eliminate or mitigate vulnerabilities consistent with other design and operational considerations. SSE supports the development of programs and standards to provide life cycle security for critical defense resources.
MIL-HDBK-1791, MILITARY HANDBOOK DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT (17 FEB 1997) (SUPERSEDES MIL-STD-1791)
MIL-HDBK-1791, MILITARY HANDBOOK DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT (17 FEB 1997) (SUPERSEDES MIL-STD-1791)., This standard covers general design and performance requirements of military equipment for internal air transport in military prime mission cargo aircraft and long range international segment of the Civil Reserve Air Fleet (CRAF).
Ident. Num:
MIL-HDBK-1791
Rev. Num:
-
MIL-HDBK-1791, MILITARY HANDBOOK DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT (17 FEB 1997) (SUPERSEDES MIL-STD-1791)., This standard covers general design and performance requirements of military equipment for internal air transport in military prime mission cargo aircraft and long range international segment of the Civil Reserve Air Fleet (CRAF).
MIL-HDBK-1793 (NOTICE 1), DEPARTMENT OF DEFENSE HANDBOOK FLIGHT PERFORMANCE, AIR VEHICLE (29 MAY 2003) [SUPERSEDING MIL-STD-1793 (USAF)] [REFER TO MI
MIL-HDBK-1793 (NOTICE 1), DEPARTMENT OF DEFENSE HANDBOOK FLIGHT PERFORMANCE, AIR VEHICLE (29 MAY 2003) [SUPERSEDING MIL-STD-1793 (USAF)] [REFER TO MIL-STD-3013]., MIL-HDBK-1793 (USAF), dated 16 December 1997, is hereby cancelled. However, users may refer to the technical information and lessons learned from this handbook incorporated into MIL-STD-3013.
Ident. Num:
MIL-HDBK-1793
Rev. Num:
-
MIL-HDBK-1793 (NOTICE 1), DEPARTMENT OF DEFENSE HANDBOOK FLIGHT PERFORMANCE, AIR VEHICLE (29 MAY 2003) [SUPERSEDING MIL-STD-1793 (USAF)] [REFER TO MIL-STD-3013]., MIL-HDBK-1793 (USAF), dated 16 December 1997, is hereby cancelled. However, users may refer to the technical information and lessons learned from this handbook incorporated into MIL-STD-3013.
MIL-HDBK-1797A, DEPARTMENT OF DEFENSE HANDBOOK FLYING QUALITIES OF PILOTED AIRCRAFT (19 DEC 1997) (SUPERSEDING MIL-STD-1797A)
MIL-HDBK-1797A, DEPARTMENT OF DEFENSE HANDBOOK FLYING QUALITIES OF PILOTED AIRCRAFT (19 DEC 1997) (SUPERSEDING MIL-STD-1797A)., This standard is intended for use with fixed-wing aircraft supported primarily by aerodynamic force rather than engine thrust. It also covers the handling characteristics of aircraft under piloted control on the ground, and may be used with powered-lift aircraft in aerodynamic flight (above the conversion speed, Vcon). This standard also applies to piloted transatmospheric flight when flight depends upon aerodynamic lift and/or air breathing propulsion systems. Flying qualities of military rotorcraft are specified in MIL-H- 8501. while flying qualities in V/STOL flight are the subject of MIL-F-83300. NOTE: MIL-STD-1797A has been redesignated as a handbook, and is to be used for guidance purposes only. This document is no longer to be cited as a requirement. For administrative expediency, the only physical change from MIL-STD-1797A is this cover page. However, this document is no longer to be cited as a requirement. If cited as a requirement, contractors may disregard the requirements of this document and interpret its contents only as guidance. For further background information, see Appendix C.
Ident. Num:
MIL-HDBK-1797
Rev. Num:
-
MIL-HDBK-1797A, DEPARTMENT OF DEFENSE HANDBOOK FLYING QUALITIES OF PILOTED AIRCRAFT (19 DEC 1997) (SUPERSEDING MIL-STD-1797A)., This standard is intended for use with fixed-wing aircraft supported primarily by aerodynamic force rather than engine thrust. It also covers the handling characteristics of aircraft under piloted control on the ground, and may be used with powered-lift aircraft in aerodynamic flight (above the conversion speed, Vcon). This standard also applies to piloted transatmospheric flight when flight depends upon aerodynamic lift and/or air breathing propulsion systems. Flying qualities of military rotorcraft are specified in MIL-H- 8501. while flying qualities in V/STOL flight are the subject of MIL-F-83300. NOTE: MIL-STD-1797A has been redesignated as a handbook, and is to be used for guidance purposes only. This document is no longer to be cited as a requirement. For administrative expediency, the only physical change from MIL-STD-1797A is this cover page. However, this document is no longer to be cited as a requirement. If cited as a requirement, contractors may disregard the requirements of this document and interpret its contents only as guidance. For further background information, see Appendix C.
MIL-HDBK-1798 (NOTICE 1), DEPARTMENT OF DEFENSE HANDBOOK MECHANICAL EQUIPMENT AND SUBSYSTEMS INTEGRITY PROGRAM (19 DEC 1997) (SUPERSEDING MIL-STD-1798
MIL-HDBK-1798 (NOTICE 1), DEPARTMENT OF DEFENSE HANDBOOK MECHANICAL EQUIPMENT AND SUBSYSTEMS INTEGRITY PROGRAM (19 DEC 1997) (SUPERSEDING MIL-STD-1798)., The purpose of this standard is to describe the general process (program) to achieve and maintain the integrity of aerospace and ground mission mechanical systems, subsystems, and equipment.
Ident. Num:
MIL-HDBK-1798
Rev. Num:
-
MIL-HDBK-1798 (NOTICE 1), DEPARTMENT OF DEFENSE HANDBOOK MECHANICAL EQUIPMENT AND SUBSYSTEMS INTEGRITY PROGRAM (19 DEC 1997) (SUPERSEDING MIL-STD-1798)., The purpose of this standard is to describe the general process (program) to achieve and maintain the integrity of aerospace and ground mission mechanical systems, subsystems, and equipment.
