NASA STD 6008 : 2008 CHANGE 1 2013
|
NASA FASTENER PROCUREMENT, RECEIVING INSPECTION, AND STORAGE PRACTICES FOR SPACEFLIGHT HARDWARE |
NASM85604:2012
|
BOLT, NICKEL ALLOY 718, TENSION, HIGH STRENGTH, 125 KSI FSU AND 220 KSI FTU, HIGH TEMPERATURE, SPLINE DRIVE |
NASA STD 5020 : 2012
|
REQUIREMENTS FOR THREADED FASTENING SYSTEMS IN SPACEFLIGHT HARDWARE |
NASA PRC 6509 : 2011
|
PROCESS SPECIFICATION FOR EDDY CURRENT INSPECTION |
NASM1312-11:2017
|
FASTENER TEST METHODS METHOD 11 TENSION FATIGUE |
NASA STD 5001 : 2014
|
STRUCTURAL DESIGN AND TEST FACTORS OF SAFETY FOR SPACEFLIGHT HARDWARE |
NASA STD 5017 : 2015
|
DESIGN AND DEVELOPMENT REQUIREMENTS FOR MECHANISMS |
SAE AS 7468 : 2012
|
BOLTS, COBALT-CHROMIUM-NICKEL ALLOY, UNS R30035, TENSILE STRENGTH 260 KSI, PROCUREMENT SPECIFICATION |
NA 0271 : REV 2
|
PROCUREMENT SPECIFICATION, METRIC FASTENERS, CRES 300 SERIES, EXTERNALLY THREADED, MJ THREAD, 500 MPA FTU AND 700 MPA FTU |
NASA HDBK 5010 : 0
|
FRACTURE CONTROL IMPLEMENTATION HANDBOOK FOR PAYLOADS, EXPERIMENTS, AND SIMILAR HARDWARE |
NASA MSFC STD 3029 : 2000
|
GUIDELINES FOR THE SELECTION OF METALLIC MATERIALS FOR STRESS CORROSION CRACKING RESISTANCE IN SODIUM CHLORIDE ENVIRONMENTS |
NASA MSFC RQMT 3479 : 2006
|
FRACTURE CONTROL REQUIREMENTS FOR COMPOSITE AND BONDED VEHICLE AND PAYLOAD STRUCTURES |
ASTM E 2899 : 2015 : REDLINE
|
Standard Test Method for Measurement of Initiation Toughness in Surface Cracks Under Tension and Bending |
NASA STD 5018 : 2011
|
STRENGTH DESIGN AND VERIFICATION CRITERIA FOR GLASS, CERAMICS, AND WINDOWS IN HUMAN SPACE FLIGHT APPLICATIONS |
NA 0026 : REV 3
|
PROCUREMENT SPECIFICATION, METRIC FASTENERS, A-286 CRES EXTERNALLY THREADED, 1100 MPA TENSILE, 660 MPA SHEAR |
NAM 1312/111 : REV 1
|
FASTENER TEST METHODS, METRIC METHOD 111 TENSION FATIGUE |
API 579-1 : 2016
|
FITNESS-FOR-SERVICE |
MIL-HDBK-6870 Revision B:2012
|
NONDESTRUCTIVE INSPECTION PROGRAM REQUIREMENTS FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS |
NAS 4003 : 2003
|
FASTENER, A286 CORROSION RESISTANT ALLOY, EXTERNALLY THREADED, 160 KSI FTU, 95 KSI FSU, 1000 DEGREES F |
NASA STD 6016 : 2016
|
STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT |
NASA STD 5009 : 2008
|
NONDESTRUCTIVE EVALUATION REQUIREMENTS FOR FRACTURE-CRITICAL METALLIC COMPONENTS - MEASUREMENT SYSTEM IDENTIFICATION: METRIC (INCH-POUND) |
NASA JSC 20793 : 2017
|
CREWED SPACE VEHICLE BATTERY SAFETY REQUIREMENTS |