Union Catalogue of Belgian Libraries
Listing 1 - 10 of 30
|
<<
page
>>
|
Sort by
|
Book
The effect of impact damage next to holes on the bearing strength of carbon fiber laminates
![](/uniCatImages/spinner.gif)
Loading...
Export citation
Choose an application
Book
Permeability testing of impacted composite laminates for use on reusable launch vehicles
![](/uniCatImages/spinner.gif)
Loading...
Export citation
Choose an application
Book
A damage tolerance comparison of composite hat-stiffened and honeycomb sandwich structure for launch vehicle interstage applications
![](/uniCatImages/spinner.gif)
Loading...
Export citation
Choose an application
Book
Hot/wet open hole compression strength of carbon/epoxy laminates for launch vehicle applications
![](/uniCatImages/spinner.gif)
Loading...
Export citation
Choose an application
Book
A brief overview of the effects of impact damage to rocket motor cases
![](/uniCatImages/spinner.gif)
Loading...
Export citation
Choose an application
Book
The effects of compressive preloads on the compression-after-impact strength of carbon/epoxy
Authors:
Nettles, A. T.
---
Lance, D. G.
---
United States.
Year: 1992
Publisher: [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical, Information Program,
![](/uniCatImages/spinner.gif)
Loading...
Export citation
Choose an application
Book
A brief overview of the effects of impact damage to rocket motor cases
![](/uniCatImages/spinner.gif)
Loading...
Export citation
Choose an application
Book
The effect of impact damage next to holes on the bearing strength of carbon fiber laminates
![](/uniCatImages/spinner.gif)
Loading...
Export citation
Choose an application
Book
The effects of compressive preloads on the compression-after-impact strength of carbon/epoxy
Authors:
Nettles, A. T.
---
Lance, D. G.
---
United States.
Year: 1992
Publisher: [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical, Information Program,
![](/uniCatImages/spinner.gif)
Loading...
Export citation
Choose an application
Book
A damage tolerance comparison of composite hat-stiffened and honeycomb sandwich structure for launch vehicle interstage applications
![](/uniCatImages/spinner.gif)
Loading...
Export citation
Choose an application
Listing 1 - 10 of 30
|
<<
page
>>
|
Sort by
|