NASA HDBK 5010 : 0
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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FRACTURE CONTROL IMPLEMENTATION HANDBOOK FOR PAYLOADS, EXPERIMENTS, AND SIMILAR HARDWARE
Hardcopy , PDF
21-09-2024
English
24-05-2005
Important note : Users cannot be edited or removed once added to your Multi user PDF.
DOCUMENT HISTORY LOG
ACKNOWLEDGEMENTS
FOREWORD
1 INTRODUCTION
2 PURPOSE
3 RESPONSIBILITIES
4 APPLICABLE/REFERENCE DOCUMENTS/WEBSITE
5 FRACTURE CONTROL CLASSIFICATION OF PARTS/COMPONENTS
6 METHODOLOGY FOR ASSESSING FRACTURE CRITICAL HARDWARE
7 TRACKING FOR FRACTURE CRITICAL PARTS
8 FRACTURE CONTROL DOCUMENTATION
9 ALTERNATIVES
10 OTHER REQUIREMENTS
APPENDICES
A - ACRONYMS/DEFINITIONS
B - CONTAINMENT
C - ASSISTANCE IN DETERMINING NON-HAZARDOUS LEAK BEFORE
BURST (NHLBB) FOR PRESSURE SYSTEM COMPONENTS
D - THE GSFC EQUIVALENT LOAD SPECTRUM
E - PART FRACTURE CONTROL CLASSIFICATION PROCESS
F - STANDARD NDE GEOMETRIES AND FLAW SIZES
G - PRESSURIZED HARDWARE
H - FRACTURE ASSESSMENT CHECK SHEETS
I - POST PROOF TEST INSPECTION OF PRESSURE VESSELS AND
HABITABLE MODULES
J - DIMENSIONS FOR FRACTURE CONTROL ANALYSES
K - FRACTURE CRITICAL CLASSIFICATION OF ROTATING HARDWARE
WITH KINETIC ENERGY LESS THAN 14,240 FOOT-POUNDS
L - FRACTURE CONTROL PLAN EXAMPLE 1, VAPOR COMPRESSION
DISTILLATION FLIGHT EXPERIMENTS (VCDFE)
M - FRACTURE CONTROL PLAN EXAMPLE 2, INTEGRATED HABITAT
HOLDING RACK 1 (IHHR1)
N - FRACTURE CONTROL SUMMARY REPORT (FCSR) EXAMPLE
O - FRACTURE CONTROL PRESENTATION EXAMPLE
P - DETAILED FRACTURE CONTROL ANALYSIS REPORT EXAMPLE
INDEX
Reflects many years of implementation experience related to fracture control assessment of hardware that has flown abroad the NASA Space Shuttle.
| DocumentType |
Standard
|
| Pages |
233
|
| PublisherName |
National Aeronautics and Space Administration
|
| Status |
Superseded
|
| SupersededBy |
| NASA SP 3421 : 2011 | PROBABILISTIC RISK ASSESSMENT PROCEDURES GUIDE FOR NASA MANAGERS AND PRACTITIONERS |
| I.S. EN 16603-32-01:2014 | SPACE ENGINEERING - FRACTURE CONTROL |
| BS EN 16603-32-01:2014 | Space engineering. Fracture control |
| NASA MSFC RQMT 3479 : 2006 | FRACTURE CONTROL REQUIREMENTS FOR COMPOSITE AND BONDED VEHICLE AND PAYLOAD STRUCTURES |
| NASA STD 5019 : 2016 | FRACTURE CONTROL REQUIREMENTS FOR SPACEFLIGHT HARDWARE |
| NASA STD 5019(INT) : 2006 | FRACTURE CONTROL REQUIREMENTS FOR SPACEFLIGHT HARDWARE |
| NASA JSC 25863 : 2009 | FRACTURE CONTROL PLAN FOR JSC SPACE-FLIGHT HARDWARE |
| EN 16603-32-01:2014 | Space engineering - Fracture control |
| MIL-STD-1522 Revision A:1984 | STANDARD GENERAL REQUIREMENTS FOR SAFE DESIGN AND OPERATION OF PRESSURIZED MISSILE AND SPACE SYSTEMS |
| NASA STD 5001 : 2014 | STRUCTURAL DESIGN AND TEST FACTORS OF SAFETY FOR SPACEFLIGHT HARDWARE |
| ASTM E 1823 : 2013-07 | TERMINOLOGY RELATING TO FATIGUE AND FRACTURE TESTING |
| NASA STD 7001 : 2011 | PAYLOAD VIBROACOUSTIC TEST CRITERIA |
| NASA STD 5003 : 0 | FRACTURE CONTROL REQUIREMENTS FOR PAYLOADS USING THE SPACE SHUTTLE |
| NASA STD 5009 : 2008 | NONDESTRUCTIVE EVALUATION REQUIREMENTS FOR FRACTURE-CRITICAL METALLIC COMPONENTS - MEASUREMENT SYSTEM IDENTIFICATION: METRIC (INCH-POUND) |
| NASA STD 5007 : 2001 | GENERAL FRACTURE CONTROL REQUIREMENTS FOR MANNED SPACEFLIGHT SYSTEMS |
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