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-STD-129 Revision R:2014
|
Military Marking for Shipment and Storage |
MIL-F-8785 Revision C:1980
|
FLYING QUALITIES OF PILOTED AIRPLANES |
MIL-STD-2088 Revision B:2007
|
BOMB RACK UNIT (BRU), SINGLE STORE, AIRCRAFT |
STANAG 3791 : 1999
|
INTEROPERABILITY OF NATO AIRCRAFT AND STORES - AOP-11 |
MIL-STD-704 Revision F:2004
|
AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
MIL-A-8863 Revision C:1993
|
AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES |
STANAG 3837 : 0
|
AIRCRAFT STORES ELECTRICAL INTERCONNECTION SYSTEM |
MIL-STD-220 Revision C:2009
|
TEST METHOD STANDARD - METHOD OF INSERTION LOSS MEASUREMENT |
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-A-8869 Revision B:1987
|
AIRPLANE STRENGTH AND RIGIDITY NUCLEAR WEAPONS EFFECTS |
DOD STD 1686 : 0
|
ELECTROSTATIC DISCHARGE CONTROL PROGRAM FOR PROTECTION OF ELECTRICAL AND ELECTRONIC PARTS ASSEMBLIES AND EQUIPMENT (EXCLUDING ELECTRICALLY INITIATED EXPLOSIVE DEVICES)(METRIC) |
STANAG 3525 : 0
|
SAFETY DESIGN REQUIREMENTS - AIRBORNE FUZING SYSTEMS |
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-1316 Revision F:2017
|
Fuze Design, Safety Criteria for |
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] |
STANAG 3898 : 2009
|
AIRCRAFT STORES INTERFACE MANUAL (ASIM) - AOP-12 |
MIL I 23659 : C
|
INITIATOR, ELECTRIC, GENERAL DESIGN SPECIFICATION |
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 C 38999 : J
|
CONNECTOR, ELECTRICAL, CIRCULAR, MINIATURE, HIGH DENSITY, QUICK DISCONNECT (BAYONET THREADED & BREECH COUPLING) ENVIRONMENT RESISTANT, REMOVABLE CRIMP & HERMETIC SOLDER CONTACTS |
DOD HDBK 263 : LATEST
|
ELECTROSTATIC DISCHARGE CONTROL HANDBOOK FOR PROTECTION OF ELECTRICAL AND ELECTRONIC PARTS, ASSEMBLIES AND EQUIPMENT (EXCLUDING ELECTRICALLY INITIATED EXPLOSIVE DEVICES)METRIC |
STANAG 3575 : 0
|
AIRCRAFT STORES EJECTOR RACKS |
MIL-E-5007 Revision D:1973
|
ENGINE, AIRCRAFT, TURBOJET AND TURBOFAN, GENERAL SPECIFICATION FOR |
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 F 15733 : G
|
FILTERS & CAPACITORS, RADIO FREQUENCY INTERFERENCE |
STANAG 3726 : 1996
|
BAIL (PORTAL) LUGS FOR THE SUSPENSION OF AIRCRAFT STORES |
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 1763 : A
|
AIRCRAFT STORES CERTIFICATION PROCEDURES |
MIL-A-8867 Revision C:1987
|
AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS |
MIL-D-81303 Revision A:1966
|
DESIGN AND EVALUATION OF CARTRIDGES FOR STORES SUSPENSION EQUIPMENT |
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-1472 Revision G:2012
|
HUMAN ENGINEERING |
MIL-STD-1319 Revision A:1976
|
ITEM CHARACTERISTICS AFFECTING TRANSPORTABILITY AND PACKAGING AND HANDLING EQUIPMENT DESIGN |
STANAG 3899 : 0
|
GROUND FIT AND COMPATIBILITY CRITERIA FOR AIRCRAFT STORES |
MIL-D-8708 Revision C:1991
|
DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
MIL A 87221 : 0
|
AIRCRAFT STRUCTURES, GENERAL SPECIFICATION FOR REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
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-H-8501 Revision A:1961
|
HELICOPTER FLYING AND GROUND HANDLING QUALITIES, GENERAL REQUIREMENTS FOR (AF USE MIL F 83300) |
MIL-B-5087 Revision B:1964
|
BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS |
MIL-S-8698 Base Document:1954
|
STRUCTURAL DESIGN REQUIREMENTS, HELICOPTERS [ASG] |
MIL-STD-1289 Revision D:2003
|
AIRBORNE STORES GROUND FIT AND COMPATIBILITY, REQUIREMENTS |
STANAG 3842 : 2008
|
RAIL LAUNCHED MISSILE/LAUNCHER MECHANICAL INTERFACE |
MIL-M-8856 Revision B:1990
|
MISSILE, GUIDED, STRUCTURAL INTEGRITY, GENERAL SPECIFICATION FOR |
MIL-A-8860 Revision B:1987
|
AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR |
MIL-STD-1553 Revision B:1978
|
DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA |