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Lightweight structural design of a bolted case joint for the space shuttle solid rocket motor
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Stein, Peter A. Dorsey, John T. Bush, Harold G. |
| Copyright Year | 1988 |
| Description | The structural design of a bolted joint with a static face seal which can be used to join Space Shuttle Solid Rocket Motor (SRM) case segments is given. Results from numerous finite element parametric studies indicate that the bolted joint meets the design requirement of preventing joint opening at the O-ring locations during SRM pressurization. A final design recommended for further development has the following parameters: 180 one-in.-diam. studs, stud centerline offset of 0.5 in radially inward from the shell wall center line, flange thickness of 0.75 in, bearing plate thickness of 0.25 in, studs prestressed to 70 percent of ultimate load, and the intermediate alcove. The design has a mass penalty of 1096 lbm, which is 164 lbm greater than the currently proposed capture tang redesign. |
| File Size | 1254719 |
| Page Count | 26 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19890003209 |
| Archival Resource Key | ark:/13960/t83j8c53q |
| Language | English |
| Publisher Date | 1988-11-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance Finite Element Method Engine Design Space Shuttle Main Engine O Ring Seals Weight Reduction Bolted Joints Rocket Engine Cases Segments Structural Analysis Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
