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1,253 records · Page 70
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NASA NTRSDate not supplied

2021 CMH-17 Vol 5 Virtual Meeting CMC M&P Brief Overview

This overview (several slides) describes 1) the overall Goals of the CMH-17 Vol 5 CMC M&P (Materials and Processes) Working Group, 2) M&P sections in the existing CMH-17 Vol 5A that have been targeted for updating, 3) challenges to updating that content for the next edition of Vol 5, and 4) M&P plans for updating CMH-17 Vol 5A. M&P Working Group chairs Kiser and Lehman are leading a group of technical experts to address the sections that require the most attention in terms of updating information. A virtual meeting is providing an opportunity to recruit CMC, fiber, and EBC technical experts to address those sections. Goals will be defined for completing the updating of those sections, taking into account the need to have the updated content reviewed by SME (subject matter experts) well in advance of the publishing date.

Environmental Barrier Coating (EBC)↗
NASA NTRS2022

Guidebook for Assessing Similarity and Implementing Empirical Transfer Functions for Probability of Detection (POD) Demonstrations for Signal Based Nondestructive Evaluation (NDE) Methods

This document provides guidance for assessing similarity relative to nondestructive evaluation (NDE) detectability based on Probability of Detection demonstrations when comparing different NDE inspection situations. Differences in inspection situations addressed by the similarity assessment methodology herein can include differences in the component being inspected, and differences in the conditions for the inspection. Additional differences in the inspection situation relative to differences in the method or procedure are not addressed in this document but can be assessed using NDE calibration or instrument standardization specimens.

Probability of Detection↗
NASA NTRS2022

A Survey of NASA Standard Nondestructive Evaluation (NDE)

This document provides a comprehensive review to trace the evolution of NASA’s Standard nondestructive evaluation (NDE) flaw sizes provided in NASA-STD-5009B for fracture-critical metallic spaceflight hardware. A NASA Standard NDE flaw size is considered to be conservative such that most inspectors, trained and certified in the specific method, are expected to provide the required 90/95 probability of detection (POD) for that flaw size. As such, individual certified inspectors are not required to perform POD demonstration testing to be allowed to inspect fracture-critical hardware for that specific method.

Probability of Detection↗
NASA NTRS2022

Guidebook for the Design and Analysis of a NASA Standard Nondestructive Evaluation (NDE) Probability of Detection (POD) Study

Purpose: This document provides guidance on the design and analysis of a NASA Standard nondestructive evaluation (NDE) probability of detection (POD) study. A Standard NDE flaw size is considered to be conservative such that most inspectors, trained and certified in the specific NDE method, are expected to provide at least 90/95 POD for that flaw size to inspect fracture-critical hardware. Scope: This document is specifically applicable to NASA Technical Standards that establish the NDE requirements for any NASA system or component, flight or ground, where fracture control and a quantitative demonstration of POD is a requirement, including NASA-STD-5009B, Nondestructive Evaluation Requirements for Fracture-Critical Metallic Components, and NASA-STD-5019A,Fracture Control Requirements for Spaceflight Hardware.

Probability of Detection↗