NASA'S Successful "Can Crush" Will Aid Heavy-Lift Rocket Design

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March 23, 2011

Michael Braukus/J. D. Harrington 
Headquarters, Washington                                    
202-358-1979/5241 
michael.j.braukus@xxxxxxxx / j.d.harrington@xxxxxxxx 

Jennifer Stanfield 
Marshall Space Flight Center, Ala. 
256-544-0034 
jennifer.stanfield@xxxxxxxx 


RELEASE: 11-084

NASA'S SUCCESSFUL "CAN CRUSH" WILL AID HEAVY-LIFT ROCKET DESIGN

WASHINGTON -- NASA put the squeeze on a large rocket test section 
today. Results from this structural strength test at NASA's Marshall 
Space Flight Center in Huntsville, Ala., will help future heavy-lift 
launch vehicles weigh less and reduce development costs. 

This trailblazing project is examining the safety margins needed in 
the design of future, large launch vehicle structures. Test results 
will be used to develop and validate structural analysis models and 
generate new "shell-buckling knockdown factors" -- complex 
engineering design standards essential to launch vehicle design. 

"This type of research is critical to NASA developing a new heavy-lift 
vehicle," said NASA Administrator Charlie Bolden. "The Authorization 
Act of 2010 gave us direction to take the nation beyond low-Earth 
orbit, but it is the work of our dedicated team of engineers and 
researchers that will make future NASA exploration missions a 
reality." 

The aerospace industry's shell buckling knockdown factors date back to 
Apollo-era studies when current materials, manufacturing processes 
and high-fidelity computer modeling did not exist. These new analyses 
will update essential design factors and calculations that are a 
significant performance and safety driver in designing large 
structures like the main fuel tank of a future heavy-lift launch 
vehicle. 
During the test, a massive 27.5-foot-diameter and 20-foot-tall 
aluminum-lithium test cylinder received almost one million pounds of 
force until it failed. More than 800 sensors measured strain and 
local deformations. In addition, advanced optical measurement 
techniques were used to monitor tiny deformations over the entire 
outer surface of the test article. 

The Shell Buckling Knockdown Factor Project is led by engineers at 
NASA's Engineering and Safety Center (NESC), and NASA's Langley 
Research Center in Hampton, Va. NASA's heavy-lift space launch system 
will be developed and managed at Marshall. 

"Launch vehicles are thin walled, cylindrical structures and buckling 
is one of the primary failure modes," said Mark Hilburger, a senior 
research engineer in the Structural Mechanics and Concepts Branch at 
Langley and the principal investigator of the NESC's Shell Buckling 
Knockdown Factor project. "Only by studying the fundamental physics 
of buckling through careful testing and analysis can we confidently 
apply the new knowledge to updated design factors. The outcome will 
be safer, lighter, more efficient launch vehicles." 

Leading up to this full-scale test, the shell buckling team tested 
four, 8-foot-diameter aluminum-lithium cylinders. Current research 
suggests applying the new design factors and incorporating new 
technology could reduce the weight of large heavy-lift launch 
vehicles by as much as 20 percent. 

"Marshall's Structural and Dynamics Engineering Test laboratory is 
uniquely suited for shell buckling testing," said Mike Roberts, an 
engineer in Marshall's structural strength test branch and the center 
lead for this activity. "Originally built to test Saturn rocket 
stages, the capabilities found here were essential to developing the 
lightweight space shuttle external tank flying today and for testing 
International Space Station modules." 

For this test, Marshall led all test operations including the 
engineering, test equipment design and safety assurance. Lockheed 
Martin Space Systems Company fabricated the test article at 
Marshall's Advance Weld Process Development Facility using 
state-of-the-art welding and inspection techniques. Langley engineers 
led the design and analysis of the test articles, defined the test 
requirements, and developed new optical displacement measurement 
standards that enabled highly accurate assessment of the large-scale 
test article response during the test. 

In the future, the shell buckling team will test carbon-fiber 
composite structures that are 20-30 percent lighter than aluminum and 
widely used in the automotive and aerospace industries. 

For more information, visit: 



http://www.nasa.gov/exploration 


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