MIL-D-8684 Revision B:1959
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
DATA AND TESTS, ENGINEERING, CONTACT REQUIREMENTS FOR AIR LAUNCHED GUIDED MISSILE SYSTEMS
28-08-1996
English
Important note : Users cannot be edited or removed once added to your Multi user PDF.Covers requirements for engineering data and tests to be furnished under contracts for air launched guided missile systems.
| Committee |
FSC 14GP
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| DocumentType |
Standard
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| Pages |
91
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Withdrawn
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| MIL-STD-1606 Revision A:1983 | TECHNICAL INFORMATION REQUIREMENTS FOR AIR LAUNCHED GUIDED MISSILE PROPOSALS |
| MIL STD 1304 : A | RELIABILITY AND MAINTAINABILITY ENGINEERING DATA |
| MIL-I-8500 Revision D:1980 | INTERCHANGEABILITY AND REPLACEABILITY OF COMPONENT PARTS FOR AEROSPACE VEHICLES |
| MIL D 5480 : F | DATA, ENGINEERING AND TECHNICAL REPRODUCTION REQUIREMENTS FOR |
| MIL M 8910 : NOTICE 1 | MANUALS, TECHNICAL, ILLUSTRATED PARTS BREAKDOWN |
| MIL-STD-704 Revision F:2004 | AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
| MIL-H-25475 Revision B:1971 | HYDRAULIC SYSTEM, MISSILE, DESIGN, INSTALLATION TESTS AND DATE REQUIREMENTS, GENERAL REQUIREMENTS FOR |
| MIL-A-8870 Revision C:1993 | AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE |
| MIL-E-7016 Revision F:1976 | ELECTRIC LOAD AND POWER SOURCE CAPACITY, AIRCRAFT ANALYSIS OF |
| MIL STD 15 : (2) | ELECTRICAL WIRING EQUIPMENT SYMBOLS FOR SHIPS PLANS PART 2 |
| MIL E 5400 : T | ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR |
| MIL-W-3947 Revision B:1969 | Weight and Balance Control System For Guided Missiles and Space Launch Vehicles (Use SAWE-RP9) |
| MIL-STD-838 Revision C:1983 | LUBRICATION OF MILITARY EQUIPMENT |
| MIL-STD-176 Revision A:1963 | GUIDED MISSILES AND SPACE LAUNCH VEHICLES, WEIGHT AND BALANCE DATA REPORTING FORMS FOR |
| MIL-A-8868 Revision B:1987 | AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS |
| MIL-T-5422 Revision F:1971 | TESTING, ENVIRONMENTAL, AIRCRAFT ELECTRONIC EQUIPMENT |
| MIL S 901 : D | SHOCK TESTS, HI [HIGH IMPACT] SHIPBOARD MACHINERY, EQUIPMENT AND SYSTEMS, REQUIREMENTS FOR |
| MIL-P-25062 Revision B:1964 | Parachute Recovery System, Missile and Drone, General Requirements for Development of |
| MIL-STD-100 Revision G:1997 | ENGINEERING DRAWINGS |
| MIL-D-18300 Revision H:1993 | DESIGN EXAMINATIONS, ENGINEERING AVIONIC SYSTEMS/EQUIPMENT GENERAL REQUIREMENTS FOR |
| MIL-STD-167 Base Document:1993 | MECHANICAL VIBRATIONS OF SHIPBOARD EQUIPMENT |
| MIL-E-8189 Revision H:1975 | ELECTRONIC EQUIPMENT, MISSILES, BOOSTERS AND ALLIED VEHICLES, GENERAL SPECIFICATION FOR |
| MIL-D-23660 Revision A:1965 | DATA, TECHNICAL FOR ROCKET MOTORS |
| MIL D 1000/1 : LATEST | DRAWING, ENGINEERING & ASSOCIATED DATA |
| MIL-D-18243 Revision B:1977 | Demonstration of Airborne Target and Missile Systems General Specifications for |
| MIL-F-7179 Revision G:1993 | FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM |
| MIL-S-23069 Revision A:1983 | SAFETY REQUIREMENTS, MINIMUM, FOR AIR LAUNCHED GUIDED MISSILES |
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