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MIL-HDBK-1763 Base Document:1998

Current

Current

The latest, up-to-date edition.

AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES

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English

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1 SCOPE
1.1 Scope
1.2 Purpose
1.3 Application
1.3.1 Applying the handbook
1.3.2 Applying the appendix tests and engineering data
         requirements
1.3.3 Application guidance
1.3.4 Method of reference
2 APPLICABLE DOCUMENTS
2.1 General
2.2 Government documents
2.2.1 Specifications, standards and handbooks
2.2.2 Other government documents, drawings and publications
2.3 Non-government publications
2.4 Order of precedence
3 DEFINITIONS
3.1 Standardization of terminology
3.1.1 Aircraft
3.1.2 Aircraft-stores compatibility
3.1.3 Aircraft-store
3.1.4 All-up-round (AUR)
3.1.5 Ballistics
3.1.5.1 Free-stream ballistics
3.1.5.2 Separation effects
3.1.5.3 Ballistics accuracy evaluation and verification
3.1.5.4 Ballistic trajectory
3.1.6 Carriage
3.1.6.1 Symmetrical carriage
3.1.6.2 Asymmetrical carriage
3.1.6.3 Conformal (or tangential) carriage
3.1.6.4 Multiple carriage
3.1.6.5 Single carriage
3.1.6.6 Tandem carriage
3.1.7 Authorized download
3.1.8 Compatibility engineering data package (CEDP)
3.1.9 Circular error probable (CEP)
3.1.10 Agencies
3.1.10.1 Certification agency
3.1.10.2 Compatibility agency
3.1.11 Certification of a store or airworthiness qualification
         (for army)
3.1.12 Critical conditions
3.1.13 Developmental test and evaluation (DT&E)
3.1.14 Dispersion
3.1.14.1 Aircraft dispersion
3.1.14.2 Ballistic dispersion
3.1.14.3 System dispersion
3.1.15 Electromagnetic compatibility (EMC)
3.1.15.1 Electromagnetic environment effects (E3)
3.1.15.2 Electromagnetic interference (EMI)
3.1.16 Employment
3.1.16.1 Release
3.1.16.2 Launch
3.1.16.3 Fire
3.1.16.4 Dispense
3.1.17 Failure mode
3.1.18 Flight clearance/clearance recommendation
3.1.19 Free flight (of a store)
3.1.19.1 g-jump
3.1.20 Hung store of hangfire (for army)
3.1.21 Interval
3.1.22 Mean point of impact (MPI)
3.1.23 Mixed load
3.1.24 Operating limitation
3.1.25 Operational test and evaluation (OT&E)
3.1.26 Range bias
3.1.27 Safe escape/safe arming
3.1.28 Separation
3.1.28.1 Safe separation
3.1.28.2 Acceptable separation
3.1.28.3 Pair
3.1.28.4 Ripple (or train)
3.1.28.5 Salvo
3.1.28.6 Multiple
3.1.28.7 Quantity
3.1.28.8 Selective jettison
3.1.28.9 Emergency jettison
3.1.29 Submunition
3.1.30 Suspension equipment
3.1.31 Technical manuals
4 GENERAL REQUIREMENTS
4.1 Compatibility assessment/analyses
4.1.1 General
4.1.2 Data Required
4.1.3 Physical compatibility review
4.1.3.1 Review objective
4.1.3.2 Physical deficiency
4.1.4 Engineering analyses
4.1.4.1 General
4.1.4.2 Structural analysis
4.1.4.3 Aerodynamic analysis
4.1.4.4 Aeroelastic analysis
4.1.4.5 Separation analysis
4.1.4.6 Environmental analysis
4.1.4.7 Store propulsion analysis
4.1.4.8 Shipboard suitability analysis
4.1.4.9 Target acquisition analysis for guided weapons
4.1.4.10 Gun gas analysis
4.1.4.11 Thermal analysis
4.1.4.12 Ballistic analysis
4.1.4.13 Safe escape analysis
4.1.4.14 Electromagnetic analysis
4.1.5 Results of engineering analyses
4.1.5.1 Determination
4.2 Test requirements and planning
4.2.2 Types of testing
4.2.3 Mission requirements
4.2.4 Test sequence
4.2.5 Data acquisition
4.2.6 Test planning
4.2.6.1 Explosive safety
4.3 Completion of compatibility analyses
4.3.1 Determinations
4.3.2 Certification recommendation
4.3.3 Responsibilities
4.4 Certification documentation reports
4.4.1 General
4.4.2 Report types
4.4.2.1 Data reports
4.4.2.2 Final report
4.4.2.3 Compatibility report of airworthiness qualification report
         (for the army)
5 DETAILED REQUIREMENTS
5.1 General
5.2 Test structure
5.3 Certification approval
6 NOTES
6.1 Intended use
6.2 Tailoring guidance
6.2.1 Tailoring for 1.3.1 provision
6.3 Subject term (key word) listing
6.4 International standardization agreements
TABLE
TABLE A-I Wind tunnel instrumentation requirements
TABLE A-II Recommended number of test frequencies
TABLE B-I Store mass, physical and operational characteristics
TABLE B-II Aircraft configuration characteristics
TABLE B-III Release test - aircraft flight condition data
TABLE B-IV Ballistic data definitions
TABLE B-V Ballistic data title page format
TABLE B-VI Ballistic data printout format
TABLE B-VIII Data for OFP ballistic evaluation and verification
             tests
FIGURE
FIGURE 1 Certification process
FIGURE 2 Certification process timeline
FIGURE A-1 Thermal test philosophy
FIGURE A-2 Ground test facility philosophy-wind tunnel
APPENDIX
A Ground test procedures
B Flight test procedures
C Aircraft/stores compatibility engineering data
             package

This handbook is applicable 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. These include, development, manufacturing, deployment, operations, support, training and disposal. This handbook is for guidance only and cannot be cited as a requirement. If it is, the contractor does not have to comply.

Committee
AREA MISC
DevelopmentNote
SUPERSEDING MIL-STD-1763
DocumentType
Standard
Pages
221
PublisherName
US Military Specs/Standards/Handbooks
Status
Current
Supersedes

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DEFSTAN 00-970(PT0)/17(2016) : 2016 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/7(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/14(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/15(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/12(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/13(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/11(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/8(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/10(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/16(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
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SAE AS5716A Standard Electrical and Logical Interface for Airborne Fuzing Systems

MIL-A-8865 Revision B:1987 AIRPLANE STRENGTH AND RIGIDITY MISCELLANEOUS LOADS
MIL-T-8679 Base Document:1954 TEST REQUIREMENTS, GROUND HELICOPTER
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MIL-F-8785 Revision C:1980 FLYING QUALITIES OF PILOTED AIRPLANES
MIL-A-8863 Revision C:1993 AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES
MIL-D-23222 Revision A:1971 DEMONSTRATION REQUIREMENTS FOR HELICOPTERS
STANAG 3300 : 2004 NATO GLOSSARY OF AIRCRAFT ARMAMENT TERMS AND DEFINITIONS (ENGLISH AND FRENCH) - AAP-46
MIL-A-8591 Revision H:1990 AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE); GENERAL DESIGN CRITERIA FOR
MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
MIL-HDBK-244 Revision A:1990 GUIDE TO AIRCRAFT - STORES COMPATIBILITY
MIL-T-7743 Revision F:1993 TESTING, STORE SUSPENSION AND RELEASE EQUIPMENT, GENERAL SPECIFICATION FOR
MIL-A-8869 Revision B:1987 AIRPLANE STRENGTH AND RIGIDITY NUCLEAR WEAPONS EFFECTS
MIL-E-6051 Revision D:1967 ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM
MIL-A-8870 Revision C:1993 AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE
MIL-STD-1760 Revision E:2007 AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM
MIL-I-8672 Revision B:1969 INSTALLATION AND TEST OF AIRCRAFT PYROTECHNIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR [ASG]
MIL-STD-2105 Revision D:2011 HAZARD ASSESSMENT TESTS FOR NON-NUCLEAR MUNITIONS
MIL I 23659 : C INITIATOR, ELECTRIC, GENERAL DESIGN SPECIFICATION
MIL E 5400 : T ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR
MIL-STD-1512 Base Document:1972 ELECTROEXPLOSIVE SUBSYSTEMS, ELECTRICALLY INITIATED, DESIGN REQUIREMENTS AND TEST METHODS
MIL-I-8671 Revision D:1994 INSTALLATION OF DROPPABLE STORES AND ASSOCIATED RELEASE SYSTEMS
MIL-STD-38784 Revision A:2011 GENERAL STYLE AND FORMAT REQUIREMENTS FOR TECHNICAL MANUALS
MIL-STD-831 Base Document:1963 TEST REPORTS, PREPARATION OF
MIL-STD-464 Revision C:2010 ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS
STANAG 3859 : 0 STANDARDIZED DATA LIST FOR INTEROPERABILITY STUDIES AND CERTIFICATION OF AIRCRAFT STORES
MIL PRF 9977 : K MANUALS, TECHNICAL AND CHECKLISTS - MUNITIONS/WEAPONS LOADING PROCEDURES, NONNUCLEAR AND NUCLEAR AND PACKAGES, STANDARD DATA - MUNITIONS LOADING PROCEDURES, NONNUCLEAR
STANAG 3575 : 0 AIRCRAFT STORES EJECTOR RACKS
MIL-STD-1818 Revision A:1993 ELECTROMAGNETIC EFFECTS REQUIREMENTS FOR SYSTEMS
MIL-STD-882 Revision E:2012 System Safety
STANAG 3556 : 0 AIRCRAFT STORE EJECTOR CARTRIDGES
MIL-STD-461 Revision G:2015 REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
MIL-HDBK-1797 Base Document:1997 FLYING QUALITIES OF PILOTED AIRCRAFT
MIL-A-8868 Revision B:1987 AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS
MIL-HDBK-235-1 Revision C:2010 MILITARY OPERATIONAL ELECTROMAGNETIC ENVIRONMENT PROFILES - PART 1: GENERAL GUIDANCE
MIL-STD-498 Base Document:1994 SOFTWARE DEVELOPMENT AND DOCUMENTATION
MIL-T-5422 Revision F:1971 TESTING, ENVIRONMENTAL, AIRCRAFT ELECTRONIC EQUIPMENT
MIL-A-8867 Revision C:1987 AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS
MIL-A-8861 Revision B:1986 AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS
MIL-A-8866 Revision C:1987 AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE
MIL-STD-1670 Revision A:1976 ENVIRONMENTAL CRITERIA AND GUIDELINES FOR AIR LAUNCHED WEAPONS
STANAG 3441 : 2007 DESIGN OF AIRCRAFT STORES
MIL-D-8708 Revision C:1991 DEMONSTRATION REQUIREMENTS FOR AIRPLANES
MIL-STD-462 Revision D:1993 MEASUREMENT OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS
MIL-B-81006 Revision B:1968 BOMB, FREE FALL, DEMONSTRATION OF DISPERSION REQUIREMENTS FOR
MIL-STD-331 Revision D:2017 FUZES, IGNITION SAFETY DEVICES AND OTHER RELATED COMPONENTS, ENVIRONMENTAL AND PERFORMANCE TESTS FOR
MIL-H-8501 Revision A:1961 HELICOPTER FLYING AND GROUND HANDLING QUALITIES, GENERAL REQUIREMENTS FOR (AF USE MIL F 83300)
MIL-I-8670 Revision B:1993 INSTALLATION OF FIXED GUNS AND ASSOCIATED EQUIPMENT IN NAVAL AIRCRAFT
MIL-S-8698 Base Document:1954 STRUCTURAL DESIGN REQUIREMENTS, HELICOPTERS [ASG]
MIL-STD-1289 Revision D:2003 AIRBORNE STORES GROUND FIT AND COMPATIBILITY, REQUIREMENTS
MIL-D-18243 Revision B:1977 Demonstration of Airborne Target and Missile Systems General Specifications for
MIL-A-8860 Revision B:1987 AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR

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