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Flat-H Redundant Frangible Joint Design Evolution 2018: Feasibility Study ConclusionsThis paper reports results of an investigation into developing a single failure tolerant pyrotechnic linear separation system which features completely redundant explosive trains suitable for human spaceflight. It is a follow up to “Flat-H Redundant Frangible Joint Design Evolution 2017” and “Flat-H Redundant Frangible Joint Evolution”. The paper chronicles the history of the redundant frangible joint development program including testing, analysis, and design improvements from 2014 to the present culminating in a successful proof-of-concept prototype. The paper describes work done to address debris control and containment of combustion products. A performance optimization strategy is presented along with optimization results. Additionally a novel containment manifold design is presented with test results.
Document ID
20190025245
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
French, Jacob M.
(NASA Johnson Space Center Houston, TX, United States)
Benjamin, Andrew L.
(NASA Johnson Space Center Houston, TX, United States)
Brown, Christopher W.
(NASA Johnson Space Center Houston, TX, United States)
Diegelman, Thomas E.
(NASA Johnson Space Center Houston, TX, United States)
Hinkel, Todd J.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
May 20, 2019
Publication Date
May 15, 2019
Subject Category
Engineering (General)
Report/Patent Number
JSC-E-DAA-TN67748
Report Number: JSC-E-DAA-TN67748
Meeting Information
Meeting: IAASS Conference
Location: El Segundo, CA
Country: United States
Start Date: May 15, 2019
End Date: May 17, 2019
Sponsors: International Space Safety Foundation
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Structures
Separation Systems
Frangible Joint
Pyrotechnics
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