MIL HDBK 17-5 : 0
|
COMPOSITE MATERIALS HANDBOOK - VOLUME 5: CERAMIC MATRIX COMPOSITES |
SAE AMS 2801 : 2014
|
HEAT TREATMENT OF TITANIUM ALLOY PARTS |
SAE AMS 2404 : 2013
|
PLATING, ELECTROLESS NICKEL |
ASTM B 733 : 2015 : REDLINE
|
Standard Specification for Autocatalytic (Electroless) Nickel-Phosphorus Coatings on Metal |
SAE AMS STD 401 : 1999
|
SANDWICH CONSTRUCTIONS AND CORE MATERIALS - GENERAL TEST METHODS |
NASA STD 5020 : 2012
|
REQUIREMENTS FOR THREADED FASTENING SYSTEMS IN SPACEFLIGHT HARDWARE |
SAE AMS 2488 : 2000
|
ANODIC TREATMENT - TITANIUM AND TITANIUM ALLOYS SOLUTION PH 13 OR HIGHER |
SAE AMS 2175 : 2010
|
CASTINGS, CLASSIFICATION AND INSPECTION OF |
AWS D17.3/D17.3M : 2016
|
SPECIFICATION FOR FRICTION STIR WELDING OF ALUMINUM ALLOYS FOR AEROSPACE APPLICATIONS |
NASA STD 6001 : 2011
|
FLAMMABILITY, OFFGASSING, AND COMPATIBILITY REQUIREMENTS AND TEST PROCEDURES |
MIL-STD-810 Revision G:2008
|
ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
SAE AMS 2770 : 2015
|
HEAT TREATMENT OF WROUGHT ALUMINUM ALLOY PARTS |
AWS C3.7M/C3.7 : 2011
|
SPECIFICATION FOR ALUMINUM BRAZING |
NASA STD 6012 : 2012
|
CORROSION PROTECTION FOR SPACE FLIGHT HARDWARE |
AWS C3.6M/C3.6 : 2016
|
SPECIFICATION FOR FURNACE BRAZING |
NAS410:2003
|
NAS CERTIFICATION & QUALIFICATION OF NONDESTRUCTIVE TEST PERSONNEL |
ASTM G 88 : 2013 : REDLINE
|
Standard Guide for Designing Systems for Oxygen Service |
ASTM E 595 : 2015 : REDLINE
|
Standard Test Method for Total Mass Loss and Collected Volatile Condensable Materials from Outgassing in a Vacuum Environment |
AWS G2.4/G2.4M : 2007
|
GUIDE FOR THE FUSION WELDING OF TITANIUM AND TITANIUM ALLOYS |
AWS C3.3 : 2008
|
RECOMMENDED PRACTICES FOR THE DESIGN, MANUFACTURE, AND EXAMINATION OF CRITICAL BRAZED COMPONENTS |
SAE AMS 2759 : 2014
|
HEAT TREATMENT OF STEEL PARTS, GENERAL REQUIREMENTS |
AWS C3.5M/C3.5 : 2016
|
SPECIFICATION FOR INDUCTION BRAZING |
MIL-STD-1252 Base Document:1975
|
INERTIA FRICTION WELDING PROCESS, PROCEDURE AND PERFORMANCE QUALIFICATION |
MIL-HDBK-454 Revision B:2007
|
GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT |
AWS D17.2/D17.2M : 2013
|
SPECIFICATION FOR RESISTANCE WELDING FOR AEROSPACE APPLICATIONS |
AWS C3.4M/C3.4 : 2016
|
SPECIFICATION FOR TORCH BRAZING |
AWS C3.2M/C3.2 : 2008
|
STANDARD METHOD FOR EVALUATING THE STRENGTH OF BRAZED JOINTS |
SAE AS 22759 : 2014
|
WIRE, ELECTRICAL, FLUOROPOLYMER-INSULATED, COPPER OR COPPER ALLOY |
SAE AMS 2491 : 2015
|
SURFACE TREATMENT OF POLYTETRAFLUOROETHYLENE (PTFE), PREPARATION FOR BONDING |
SAE AMS 2423 : 2015
|
PLATING, NICKEL, HARD DEPOSIT |
SAE AMS 2680 : 2001
|
ELECTRON-BEAM WELDING, FOR FATIGUE CRITICAL APPLICATIONS |
GEIA STD 0005-2 : 2012
|
MITIGATING THE EFFECTS OF TIN WHISKERS IN AEROSPACE AND HIGH PERFORMANCE ELECTRONIC SYSTEMS |
ASTM E 2900 : 2012
|
Standard Practice for Spacecraft Hardware Thermal Vacuum Bakeout |
SAE R-427 : 2013
|
COMPOSITE MATERIALS HANDBOOK - VOLUME 6: STRUCTURAL SANDWICH COMPOSITES |
SAE AMS 2772 : 2016
|
HEAT TREATMENT OF ALUMINUM ALLOY RAW MATERIALS |
NASA STD 5019 : 2016
|
FRACTURE CONTROL REQUIREMENTS FOR SPACEFLIGHT HARDWARE |
NASA MSFC STD 3029 : 2000
|
GUIDELINES FOR THE SELECTION OF METALLIC MATERIALS FOR STRESS CORROSION CRACKING RESISTANCE IN SODIUM CHLORIDE ENVIRONMENTS |
NASA STD 5006 : 2015
|
GENERAL FUSION WELDING REQUIREMENTS FOR AEROSPACE MATERIALS |
NASA JSC 29353 : 2014
|
FLAMMABILITY CONFIGURATION ANALYSIS FOR SPACECRAFT APPLICATIONS |
SAE AMS H 81200 : 2014
|
HEAT TREATMENT OF TITANIUM AND TITANIUM ALLOYS |
SAE AMS 2759/9 : 2009
|
HYDROGEN EMBRITTLEMENT RELIEF (BAKING) OF STEEL PARTS |
NASA MSFC SPEC 445 : 1990
|
ADHESIVE BONDING, PROCESS AND INSPECTION, REQUIREMENTS FOR |
SAE AMS 2774 : 2016
|
HEAT TREATMENT, WROUGHT NICKEL ALLOY AND COBALT ALLOY PARTS |
GEIA STD 0005-1 : 2012
|
PERFORMANCE STANDARD FOR AEROSPACE AND HIGH PERFORMANCE ELECTRONIC SYSTEMS CONTAINING LEAD-FREE SOLDER |
NASA STD 5005 : 2013
|
STANDARD FOR THE DESIGN AND FABRICATION OF GROUND SUPPORT EQUIPMENT |
SAE AMS 2403 : 2015
|
PLATING, NICKEL, GENERAL PURPOSE |
SAE R-424 : 2012
|
COMPOSITE MATERIALS HANDBOOK - VOLUME 3 |
ASTM G 63 : 2015 : REDLINE
|
Standard Guide for Evaluating Nonmetallic Materials for Oxygen Service |
SAE AMS 2453 : 2015
|
LOW STRESS GRINDING OF STEEL PARTS HEAT TREATED TO 180 KSI OR OVER, AND LOW STRESS GRINDING OF CHROME PLATING APPLIED TO STEEL PARTS HEAT TREATED TO 180 KSI OR OVER |
SAE AMS 2773 : 2013
|
HEAT TREATMENT, CAST NICKEL ALLOY AND COBALT ALLOY PARTS |
SAE R-423 : 2012
|
COMPOSITE MATERIALS HANDBOOK - VOLUME 2: POLYMER MATRIX COMPOSITES: MATERIALS PROPERTIES |
SAE R-425 : 2013
|
COMPOSITE MATERIALS HANDBOOK - VOLUME 4: METAL MATRIX COMPOSITES |
MIL-HDBK-6870 Revision B:2012
|
NONDESTRUCTIVE INSPECTION PROGRAM REQUIREMENTS FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS |
SAE R-422 : 2012
|
COMPOSITE MATERIALS HANDBOOK - VOLUME 1 |
SAE AMS H 6875 : 2010
|
HEAT TREATMENT OF STEEL RAW MATERIALS |
NASA STD 5012 : 2016
|
STRENGTH AND LIFE ASSESSMENT REQUIREMENTS FOR LIQUID-FUELED SPACE PROPULSION SYSTEM ENGINES |
AIAA G 095 : 2004
|
GUIDE TO SAFETY OF HYDROGEN AND HYDROGEN SYSTEMS |
NAS 412 : 1997
|
FOREIGN OBJECT DAMAGE (FOD) PREVENTION GUIDANCE DOCUMENT |
AWS D17.1/D17.1M : 2012
|
SPECIFICATION FOR FUSION WELDING FOR AEROSPACE APPLICATIONS |
NASA STD 5009 : 2008
|
NONDESTRUCTIVE EVALUATION REQUIREMENTS FOR FRACTURE-CRITICAL METALLIC COMPONENTS - MEASUREMENT SYSTEM IDENTIFICATION: METRIC (INCH-POUND) |
AWS C7.4/C7.4M : 2008
|
PROCESS SPECIFICATION AND OPERATOR QUALIFICATION FOR LASER BEAM WELDING |