MIL-STD-401 Revision B:1967
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
SANDWICH CONSTRUCTIONS AND CORE MATERIALS, GENERAL TEST METHODS
Available format(s)
PDF
Superseded date
01-06-1999
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.Provisions and methods for testing sandwich core materials and construction for use in aircraft structures.
| DocumentType |
Standard
|
| Pages |
41
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| MIL C 8087 : C | CORE MATERIAL, FOAMED IN PLACE, URETHANE TYPE |
| MIL-L-81293 Revision A:1992 | LIGHTWEIGHT SANDWICH CONSTRUCTED PANEL (ASROC) LAUNCHER MK 112 |
| MIL-C-7438 Revision G:1985 | CORE MATERIAL, ALUMINUM, FOR SANDWICH CONSTRUCTION |
| MIL-A-23121 Revision C:1970 | AIRCREW ENVIRONMENTAL, ESCAPE AND SURVIVAL COCKPIT CAPSULE SYSTEM, GENERAL SPECIFICATION FOR |
| MIL-A-81973 Base Document:1974 | AIRCREW AUTOMATED ESCAPE SYSTEMS, TEST VEHICLES FOR GROUND TRACK PERFORMANCE TESTING, ROCKET AND/OR JET ENGINE PROPELLED; GENERAL SPECIFICATION FOR |
| MIL-A-82175 Base Document:1968 | ARMOR, BODY, FRAGMENTATION, PROTECTIVE: FOOTWEAR |
| MIL-S-9041 Revision B:1975 | SANDWICH CONSTRUCTION, PLASTIC RESIN, GLASS FABRIC BASE, LAMINATED FACINGS AND HONEYCOMB CORE FOR AIRCRAFT STRUCTURAL APPLICATIONS |
| MIL-S-25392 Revision B:1968 | Sandwich Construction, Plastic Resin, Glass Fabric Base, Laminated Facings and Polyurethane Foamed-in-Place Core, For Aircraft Structural Applications |
| MIL-E-87235 Base Document:1985 | EMERGENCY ESCAPE, AIRCRAFT (REQUEST FOR ISSUE MUST BE SENT VIA ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
| MIL-STD-1547 Revision B:1992 | ELECTRONIC PARTS, MATERIALS, AND PROCESSES FOR SPACE VEHICLES |
| MIL-R-7705 Revision B:1975 | RADOME, GENERAL SPECIFICATION FOR |
| MIL-S-29413 Revision B:1988 | SHELTER, JOINING CORRIDOR FOR |
| DIN 65067-1:1980-12 | AEROSPACE; SANDWICH STRUCTURES WITH TOP LAYERS OF FIBRE REINFORCED PLASTICS, TECHNICAL SPECIFICATION |
| MIL-S-29410 Revision B:1988 | 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 Revision B:1990 | MOBILE TEST FACILITY, GAS TURBINE ENGINE TEST SYSTEMS - GENERAL SPECIFICATION FOR |
| MIL-S-29411 Revision B:1988 | 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 Base Document:1974 | 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 Revision A:1987 | PANEL TYPE II MODULAR PLATFORM, AIRDROP |
| ASTM C 271 : 1999 | Standard Test Method for Density of Sandwich Core Materials |
| ASTM C 393 : 2000 | Standard Test Method for Flexural Properties of Sandwich Constructions |
| ASTM D 1781 : 1998 | Standard Test Method for Climbing Drum Peel for Adhesives |
| ASTM C 297 : 1994 : R1999 | Standard Test Method for Flatwise Tensile Strength of Sandwich Constructions |
| ASTM C 363 : 2000 | Standard Test Method for Delamination Strength of Honeycomb Core Materials |
| MIL-STD-105 Revision E:1989 | SAMPLING PROCEDURES AND TABLES FOR INSPECTION BY ATTRIBUTES |
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