Feasibility of a Morphing Rocket Nozzle for Thrust Vector Control based on Corrugated Composite Lami...
Feasibility of a Morphing Rocket Nozzle for Thrust Vector Control based on Corrugated Composite Laminates
About this item
Full title
Author / Creator
Publisher
Dordrecht: Springer Netherlands
Journal title
Language
English
Formats
Publication information
Publisher
Dordrecht: Springer Netherlands
Subjects
More information
Scope and Contents
Contents
The paper presents technological, experimental and numerical studies aimed at the development of a morphing nozzle in composite material with a deformable divergent section, which is designed to control the vector of thrust in rockets without using mechanisms or localized flexible joints. The nozzle design is characterized by corrugated composite w...
Alternative Titles
Full title
Feasibility of a Morphing Rocket Nozzle for Thrust Vector Control based on Corrugated Composite Laminates
Authors, Artists and Contributors
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Primary Identifiers
Record Identifier
TN_cdi_proquest_journals_2794394942
Permalink
https://devfeature-collection.sl.nsw.gov.au/record/TN_cdi_proquest_journals_2794394942
Other Identifiers
ISSN
0929-189X
E-ISSN
1573-4897
DOI
10.1007/s10443-022-10082-9
