Marshall Technical Reports Server

Qualification Testing of Solid Rocket Booster Diagonal Strut Restraint Cable Assembly Part Number 10176–0031–102/103

NASA/TM-2006–214603, Malone, T.W., Qualification Testing of Solid Rocket Booster Diagonal Strut Restraint Cable Assembly Part Number 10176–0031–102/103, George C. Marshall Space Flight Center Marshall Space Flight Center, AL 35812, National Aeronautics and Space Administration Washington, DC 20546–0001, September 2006, pp. 100, Format(s): PDF 81017k

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This Technical Memorandum presents qualification test results for solid rocket booster diagonal strut restraint cable part number 101276–00313–102/103. During flight this assembly is exposed to a range of temperatures. MIL–W–83420 shows the breaking strength of the cable as 798 kg (1,760 lb) at room temperature but does not define cable strength at the maximum temperature to which the cable is exposed during the first 2 min of flight; 669 °C (1,236 °F). The cable, which can be built from different corrosion resistant steel alloys, may also vary in its chemical, physical, and mechanical properties at temperature. Negative margins of safety were produced by analysis of the cable at temperature using standard knockdown factors. However, MSFC–HDBK–5 allows the use of a less conservative safety factor of 1.4 and knockdown factors verified by testing. Test results allowed a calculated knockdown factor of 0.1892 to be determined for the restraint cables, which provides a minimum breaking strength of 151 kg (333 lb) at 677 °C (1,250 °F) when combined with the minimum breaking strength of 0.317-cm (0.125- or 1/8-in) diameter, type 1 composition rope.
Keywords:srb diagonal strut restraint cable assembly, materials tension testing, msfc–hdbk–5, mil–w–83420
Subjects:Chemistry and Materials: Metals and Metallic Materials: Steel
ID Code:737
Deposited On:22 May 2007