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Laser holographic nondestructive testing of the nasa x-248 rocket motor
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Harris, W. J. |
| Copyright Year | 1973 |
| Description | A program to apply holography for nondestructive testing of the X-248 rocket motor was undertaken. The objective was to establish the capability of holography in detecting known unbonding between liner and propellant. Holography was performed employing stressing techniques: (1) acoustical, (2) thermal, (3) radiative, and (4) static loading. Radiative stressing was successful in locating a large area of liner/propellant unbond. The results were correlated with destructive testing. Theoretical analysis provided an understanding of motor case holography in conjunction with radiative stressing. |
| File Size | 31953277 |
| Page Count | 114 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19730008879 |
| Archival Resource Key | ark:/13960/t6vx54852 |
| Language | English |
| Publisher Date | 1973-02-28 |
| Access Restriction | Open |
| Subject Keyword | Masers Solid Propellant Rocket Engines Holography Nondestructive Tests Stress Analysis Thermal Stresses Quality Control Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |