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This article got me thinking...
How profitable, and how feasible is it to construct "critical" rocket components from composite materials? Such components being payload fairings, interstages, or as the article focuses on, propellant tanks.
Any application such components would/could be used in?
EDIT: Specifically, are there any possible future applications of composite material on a LV where it isn't already? Like that aforementioned propellant tank, since no LV uses a purely composite tank...
How profitable, and how feasible is it to construct "critical" rocket components from composite materials? Such components being payload fairings, interstages, or as the article focuses on, propellant tanks.
Any application such components would/could be used in?
![img_0505a.jpg](http://www.nasa.gov/sites/default/files/img_0505a.jpg)
EDIT: Specifically, are there any possible future applications of composite material on a LV where it isn't already? Like that aforementioned propellant tank, since no LV uses a purely composite tank...
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