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Characterization of large 2219 aluminum alloy hand forgings for the space shuttle solid rocket booster
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Brennecke, M. W. |
| Copyright Year | 1978 |
| Description | The mechanical properties, including fracture toughness, and stress corrosion properties of four types of 2219-T852 aluminum alloy hand forgings are presented. Weight of the forgings varied between 450 and 3500 lb at the time of heat treatment and dimensions exceeded the maximum covered in existing specifications. The forgings were destructively tested to develop reliable mechanical property data to replace estimates employed in the design of the Space Shuttle Solid Rocket Booster (SRB) and to establish minimum guaranteed properties for structural refinement and for entry into specification revisions. The report summarizes data required from the forgers and from the SRB Structures contractor. |
| File Size | 4019593 |
| Page Count | 118 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19790008779 |
| Archival Resource Key | ark:/13960/t5q863z10 |
| Language | English |
| Publisher Date | 1978-12-01 |
| Access Restriction | Open |
| Subject Keyword | Metallic Materials Characterization Forging Stress Corrosion Mechanical Properties Metal Working Aluminum Alloys Human Factors Engineering Fracture Strength Booster Rocket Engines Space Shuttle Boosters 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 |
