Feasibility of a Morphing Rocket Nozzle for Thrust Vector Control based on Corrugated Composite Laminates
- Location
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Deutsche Nationalbibliothek Frankfurt am Main
- ISSN
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1573-4897
- Extent
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Online-Ressource
- Language
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Englisch
- Notes
-
online resource.
- Bibliographic citation
-
Feasibility of a Morphing Rocket Nozzle for Thrust Vector Control based on Corrugated Composite Laminates ; day:7 ; month:12 ; year:2022 ; pages:1-31
Applied composite materials ; (7.12.2022), 1-31
- Creator
-
Airoldi, Alessandro
Boiocchi, Matteo
Natali, Maurizio
Mirani, Chiara
Pancrazio, Luca Di
Consiglio, Gabriele
Ballarin, Pietro
Riva, Marco
- Contributor
-
SpringerLink (Online service)
- DOI
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10.1007/s10443-022-10082-9
- URN
-
urn:nbn:de:101:1-2023021721142835223900
- Rights
-
Open Access; Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Last update
-
14.08.2025, 10:49 AM CEST
Data provider
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Associated
- Airoldi, Alessandro
- Boiocchi, Matteo
- Natali, Maurizio
- Mirani, Chiara
- Pancrazio, Luca Di
- Consiglio, Gabriele
- Ballarin, Pietro
- Riva, Marco
- SpringerLink (Online service)
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Experimental characterization of thrust production mechanisms in a magnetic nozzle ECR thruster
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Multistable morphing structures using variable stiffness laminates
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Investigation of a Variable Camber Morphing Airfoil via SMA Wire and Corrugated Structures
Experimental characterization of thrust production mechanisms in a magnetic nozzle ECR thruster
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Flexural strengthening of Reinforced Concrete (RC) Beams Retrofitted with Corrugated Glass Fiber Reinforced Polymer (GFRP) Laminates
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