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MIL C 8087 : C
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CORE MATERIAL, FOAMED IN PLACE, URETHANE TYPE
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MIL-L-81293 Revision A:1992
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LIGHTWEIGHT SANDWICH CONSTRUCTED PANEL (ASROC) LAUNCHER MK 112
|
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MIL-C-7438 Revision G:1985
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CORE MATERIAL, ALUMINUM, FOR SANDWICH CONSTRUCTION
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MIL-A-23121 Revision C:1970
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AIRCREW ENVIRONMENTAL, ESCAPE AND SURVIVAL COCKPIT CAPSULE SYSTEM, GENERAL SPECIFICATION FOR
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MIL-A-81973 Base Document:1974
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AIRCREW AUTOMATED ESCAPE SYSTEMS, TEST VEHICLES FOR GROUND TRACK PERFORMANCE TESTING, ROCKET AND/OR JET ENGINE PROPELLED; GENERAL SPECIFICATION FOR
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MIL-A-82175 Base Document:1968
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ARMOR, BODY, FRAGMENTATION, PROTECTIVE: FOOTWEAR
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MIL-S-9041 Revision B:1975
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SANDWICH CONSTRUCTION, PLASTIC RESIN, GLASS FABRIC BASE, LAMINATED FACINGS AND HONEYCOMB CORE FOR AIRCRAFT STRUCTURAL APPLICATIONS
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MIL-S-25392 Revision B:1968
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SANDWICH CONSTRUCTION, PLASTIC RESIN, GLASS FABRIC BASE, LAMINATED FACINGS AND POLYURETHANE FOAMED-IN-PLACE CORE, FOR AIRCRAFT STRUCTURAL APPLICATIONS
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MIL-E-87235 Base Document:1985
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EMERGENCY ESCAPE, AIRCRAFT (REQUEST FOR ISSUE MUST BE SENT VIA ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503
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|
MIL-STD-1547 Revision B:1992
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ELECTRONIC PARTS, MATERIALS, AND PROCESSES FOR SPACE VEHICLES
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|
MIL-R-7705 Revision B:1975
|
RADOME, GENERAL SPECIFICATION FOR
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|
MIL-S-29413 Revision B:1988
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SHELTER, JOINING CORRIDOR FOR
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DIN 65067-1:1980-12
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AEROSPACE; SANDWICH STRUCTURES WITH TOP LAYERS OF FIBRE REINFORCED PLASTICS, TECHNICAL SPECIFICATION
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MIL-S-29410 Revision B:1988
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SHELTER ASSEMBLY, RIGID GENERAL PURPOSE
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SAE AMS C 8073 : 2013
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CORE MATERIAL, PLASTIC HONEYCOMB, LAMINATED GLASS FABRIC BASE, FOR AIRCRAFT STRUCTURAL AND ELECTRONIC APPLICATIONS
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MIL-M-81957 Revision B:1990
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MOBILE TEST FACILITY, GAS TURBINE ENGINE TEST SYSTEMS - GENERAL SPECIFICATION FOR
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MIL-S-29411 Revision B:1988
|
SHELTER ASSEMBLIES, 10 FOOT AND 20 FOOT ELECTROMAGNETIC INTERFERENCE
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|
SAE AMS C 81986 : 1998
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CORE MATERIAL, PLASTIC HONEYCOMB, NYLON PAPER BASE; FOR AIRCRAFT STRUCTURAL APPLICATIONS
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MIL-C-81986 Base Document:1974
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CORE MATERIAL, PLASTIC HONEYCOMB, NYLON PAPER BASE; FOR AIRCRAFT STRUCTURAL APPLICATIONS
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|
MIL P 43184 : 0
|
PLATFORM COMPONENTS, AIR DELIVERY. MODULAR (DUAL RAIL SYSTEM), TYPE II
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|
ASTM E 1555 : 2012 : REDLINE
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Standard Specification for Structural Paste Adhesive for Sandwich Panel Repair
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|
DIN 65090:1979-07
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AEROSPACE; TEXTILE GLASS, PREIMPREGNATED FILAMENT GLASS CLOTH FROM E-GLASS (PREPREG), TECHNICAL SPECIFICATIONS
|
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ASTM E 1091 : 2013 : REDLINE
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Standard Specification for Nonmetallic Honeycomb Core for Use in Shelter Panels
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MIL C 8073 : D
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CORE MATERIAL, PLASTIC HONEYCOMB, LAMINATED CLASS FABRIC BASE, FOR AIRCRAFT STRUCTURAL AND ELECTRONIC APPLICATIONS
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NASA MSFC STD 506 : 1988
|
MATERIALS AND PROCESSES CONTROL
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|
MIL-P-43772 Revision A:1987
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PANEL TYPE II MODULAR PLATFORM, AIRDROP
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