NASA NTRS · 19900016050
Loads analysis and testing of flight configuration solid rocket motor outer boot ring segments
Abstract
The loads testing on in-house-fabricated flight configuration Solid Rocket Motor (SRM) outer boot ring segments. The tests determined the bending strength and bending stiffness of these beams and showed that they compared well with the hand analysis. The bending stiffness test results compared very well with the finite element data.
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Ahmed, Rafiq. 1990-06-01. Loads analysis and testing of flight configuration solid rocket motor outer boot ring segments. https://ntrs.nasa.gov/citations/19900016050
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