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 |
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 |