NASA/TM-2004-213282, Murphy, N.C. and Gamwell, W.R., Solid Rocket Booster Hydraulic Pump Port Cap Joint Load Testing, George C. Marshall Space Flight Center , Marshall Space Flight Center, AL 35812, National Aeronautics and Space Administration, Washington, DC 20546-0001, June 2004, pp. 48, Format(s): PDF 28250k |
The solid rocket booster uses hydraulic pumps fabricated from cast C355 aluminum alloy, with 17–4 PH stainless
steel pump port caps. Corrosion-resistant steel, MS51830 CA204L self-locking screw thread inserts are
installed into C355 pump housings, with A286 stainless steel fasteners installed into the insert to secure
the pump port cap to the housing. In the past, pump port cap fasteners were installed to a torque of 33 Nm
(300 in-lb). However, the structural analyses used a significantly higher nut factor than indicated during tests
conducted by Boeing Space Systems. When the torque values were reassessed using Boeing’s nut factor, the
fastener preload had a factor of safety of <1, with potential for overloading the joint. This paper describes how behavior was determined for a preloaded joint with a steel bolt threaded into steel inserts in aluminum parts.
Finite element models were compared with test results. For all initial bolt preloads, bolt loads increased as
external applied loads increased. For higher initial bolt preloads, less load was transferred into the bolt, due
to external applied loading. Lower torque limits were established for pump port cap fasteners and additional
limits were placed on insert axial deformation under operating conditions after seating the insert with an initial preload.
| Keywords: | srb, hydraulic pump, fastener, c355 aluminum alloy, 17–4 ph stainless steel, cres ca 204l, corrosion-resistant steel, a286 stainless steel, torque values, mechanical testing, finite element model, fem, factor of safety, fos |
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| Subjects: | Chemistry and Materials: Metals and Metallic Materials: Aluminum |
| ID Code: | 679 |
| Deposited On: | 01 October 2004 |