NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Space Shuttle Transportation (Roll-Out) Loads DiagnosticsThe Space Transportation System (STS) consists of three primary components; an Orbiter Vehicle, an External Fuel Tank, and two Solid Rocket Boosters. The Orbiter Vehicle and Solid Rocket Boosters are reusable components, and as such, they are susceptible to durability issues. Recently, the fatigue load spectra for these components have been updated to include load histories acquired during the rollout phase of the STS processing for flight. Using traditional program life assessment techniques, the incorporation of these "rollout" loads produced unacceptable life estimates for certain Orbiter structural members. As a result, the Space Shuttle System Engineering and Integration Office has initiated a program to re-assess the method used for developing the "rollout" loads and performing the life assessments. In the fall of 2003 a set of tests were preformed to provide information to either validate existing load spectra estimation techniques or generate new load spectra estimation methods. Acceleration and strain data were collected from two rollouts of a partial-stack configuration of the Space Shuttle. The partial stack configuration consists of two Solid Rocket Boosters tied together at the upper External Tank attachment locations mounted on the Mobile Launch Platform carried by a Crawler Transporter (CT). In the current analysis, the data collected from this test is examined for consistency in speed, surface condition effects, and the characterization of the forcing function. It is observed that the speed of the CT is relatively stable. The dynamic response acceleration of the partial-stack is slightly sensitive to the surface condition of the road used for transport, and the dynamic response acceleration of the partial-stack generally increases as the transport speed increases. However, the speed sensitivity is dependent on the measurement location. Finally, the character of the forcing function is narrow-banded with the primary drivers being harmonics of two CT speed dependent excitations. One source is an excitation due to the CT treads striking the road surface, and the second is unknown.
Document ID
20050081824
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Elliott, Kenny B.
(NASA Langley Research Center Hampton, VA, United States)
Buehrle, Ralph D.
(NASA Langley Research Center Hampton, VA, United States)
James, George H.
(NASA Johnson Space Center Houston, TX, United States)
Richart, Jene A.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2005
Subject Category
Launch Vehicles And Launch Operations
Meeting Information
Meeting: IMAC XXIII: Conference and Exposition on Structural Dynaics
Location: Orlando, FL
Country: United States
Start Date: January 31, 2005
End Date: February 3, 2005
Funding Number(s)
OTHER: 23-377-10-30-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available