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NASA-STD-5019 REV A W/CHG 1

FRACTURE CONTROL REQUIREMENTS FOR SPACEFLIGHT HARDWARE

inactive
Organization: NASA
Publication Date: 1 February 2016
Status: inactive
Page Count: 119
scope:

Fracture control shall be required on allhuman-rated space systems to preclude catastrophic failure. Fracture controlprovides a specialized methodology to address the consequences of naturallyoccurring and service-induced flaws, damage, or cracks in a part or structure.This document establishes the fracture control requirements for all human-ratedspaceflight systems including payloads, propulsion systems, orbital supportequipment, and planetary habitats.

Document History

NASA-STD-5019 REV A W/CHG 3
February 1, 2016
FRACTURE CONTROL REQUIREMENTS FOR SPACEFLIGHT HARDWARE
Purpose This NASA Technical Standard establishes the fracture control requirements for National Aeronautics and Space Administration (NASA) human-rated spaceflight hardware. In accordance with NASA...
NASA-STD-5019
February 1, 2016
FRACTURE CONTROL REQUIREMENTS FOR SPACEFLIGHT HARDWARE
Purpose The purpose of this NASA Technical Standard is to establish the fracture control requirements for National Aeronautics and Space Administration (NASA) human-rated spaceflight hardware. In...
NASA-STD-5019 REV A
February 1, 2016
FRACTURE CONTROL REQUIREMENTS FOR SPACEFLIGHT HARDWARE
Purpose The purpose of this NASA Technical Standard is to establish the fracture control requirements for National Aeronautics and Space Administration (NASA) human-rated spaceflight hardware. In...
NASA-STD-5019 REV A W/CHG 1
February 1, 2016
FRACTURE CONTROL REQUIREMENTS FOR SPACEFLIGHT HARDWARE
Fracture control shall be required on allhuman-rated space systems to preclude catastrophic failure. Fracture controlprovides a specialized methodology to address the consequences of...
NASA-STD-5019
January 7, 2008
FRACTURE CONTROL REQUIREMENTS FOR SPACEFLIGHT HARDWARE
Purpose Fracture control is implemented to reduce the risk of a catastrophic failure from a defect or damage. The intent of this standard is to provide fracture control requirements for spaceflight...
NASA-STD-(I)-5019
September 12, 2006
FRACTURE CONTROL REQUIREMENTS FOR SPACEFLIGHT HARDWARE
A description is not available for this item.
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References

This document references:
NASA JSC 20793 - CREWED SPACE VEHICLE BATTERY SAFETY REQUIREMENTS
Published by NASA on March 1, 2017
Purpose and Scope This requirements document is applicable to all batteries on crewed spacecraft, including vehicle, payload, and crew equipment batteries. It defines the specific provisions required...
This document references:
NASA-STD-6016 REV C W/CHG 1 - STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT
Published by NASA on November 15, 2023
This NASA Technical Standard is directed toward materials and processes (M&P) used in the design, fabrication, and testing of space program flight hardware for NASA, including but not limited to...
This document references:
NAM1312-111 - FASTENER TEST METHODS, METRIC METHOD 111 TENSION FATIGUE
Published by AIA/NAS on October 30, 2020
A description is not available for this item.
This document references:
NASM1312-11 - FASTENER TEST METHODS METHOD 11 TENSION FATIGUE
Published by AIA/NAS on April 28, 2017
Applicability. This test method establishes the procedure and equipment to be used for room temperature tension fatigue testing of bolts, screws and nuts.
This document references:
MSFC-STD-3029 - GUIDELINES FOR THE SELECTION OF METALLIC MATERIALS FOR STRESS CORROSION CRACKING RESISTANCE IN SODIUM CHLORIDE ENVIRONMENTS
Published by NASA on February 24, 2005
This document defines the design criteria that shall be used for the selection of metallic materials in order to prevent failure due to stress corrosion cracking. APPLICABILITY. The exposure...
This document references:
NASA JSC 20793 - CREWED SPACE VEHICLE BATTERY SAFETY REQUIREMENTS
Published by NASA on March 1, 2017
Purpose and Scope This requirements document is applicable to all batteries on crewed spacecraft, including vehicle, payload, and crew equipment batteries. It defines the specific provisions required...
This document references:
AIAA S-080 - Space Systems - Metallic Pressure Vessels, Pressurized Structures, and Pressure Components
Published by AIAA on March 1, 2018
This standard establishes baseline requirements for the design, analysis, manufacturing, test, and operation of metallic pressurized hardware used for aerospace systems such as spacecraft and launch...
This document references:
NASA-STD-6016 REV C W/CHG 1 - STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT
Published by NASA on November 15, 2023
This NASA Technical Standard is directed toward materials and processes (M&P) used in the design, fabrication, and testing of space program flight hardware for NASA, including but not limited to...
This document is referenced by:
NASA-STD-5012 - STRENGTH AND LIFE ASSESSMENT REQUIREMENTS FOR LIQUID-FUELED SPACE PROPULSION SYSTEM ENGINES
Published by NASA on June 16, 2016
This Standard provides strength and life assessment requirements for National Aeronautics and Space Administration (NASA) liquid-fueled space propulsion system engines. The term"life," as used in...
This document is referenced by:
NASA-SPEC-5022 - NASA MANUFACTURING AND TEST REQUIREMENTS FOR NORMALLY CLOSED PYROVALVES FOR HAZARDOUS FLIGHT SYSTEMS APPLICATIONS
Published by NASA on June 24, 2015
The purpose of this Specification is to establish andimplement the manufacturing and test requirements and applications guidelinesfor normally closed (NC) parent metal shear-section valves. The...
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