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