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Space Shuttle Program (SSP) Shock Test and Specification Experience for Reusable Flight Hardware EquipmentAs commercial companies are nearing a preliminary design review level of design maturity, several companies are identifying the process for qualifying their multi-use electrical and mechanical components for various shock environments, including pyrotechnic, mortar firing, and water impact. The experience in quantifying the environments consists primarily of recommendations from Military Standard-1540, Product Verification Requirement for Launch, Upper Stage, and Space Vehicles. Therefore, the NASA Engineering and Safety Center (NESC) formed a team of NASA shock experts to share the NASA experience with qualifying hardware for the Space Shuttle Program (SSP) and other applicable programs and projects. Several team teleconferences were held to discuss past experience and to share ideas of possible methods for qualifying components for multiple missions. This document contains the information compiled from the discussions
Document ID
20120014074
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Larsen, Curtis E.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 26, 2013
Publication Date
August 1, 2012
Subject Category
Structural Mechanics
Report/Patent Number
NASA/TM-2012-217599
NF1676L-15213
NESC-RP-12-00779
L-20172
Report Number: NASA/TM-2012-217599
Report Number: NF1676L-15213
Report Number: NESC-RP-12-00779
Report Number: L-20172
Funding Number(s)
WBS: WBS 869021.03.07.01.05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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