MIL-HDBK-1763 Base Document:1998
Current
The latest, up-to-date edition.
AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES
English
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 |
DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
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 |
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SAE AS 5716 : 2012 | 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 |
STANAG 3558 : 2002 | LOCATION OF ELECTRICAL CONNECTORS FOR AIRCRAFT STORES |
STANAG 3605 : 0 | COMPATIBILITY OF ARMING SYSTEMS AND EXPENDABLE AIRCRAFT STORES |
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 |
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MIL-HDBK-244 Revision A:1990 | GUIDE TO AIRCRAFT - STORES COMPATIBILITY |
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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 |
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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 |
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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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