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Investigation of tc-1 flight failure using power spectral analysis
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Lorenzo, C. F. |
| Copyright Year | 1976 |
| Description | During the Titan Centaur 1 test flight a failure involving at least one of the Centaur propellant boost pumps occurred. Also, neither of the boost pump speed instruments indicated pump rotation. Accelerometer data from the Titan Centaur 1 flight failure were analyzed using power spectral density methods to determine boost pump speed during attempted starts of the Centaur. The technique was demonstrated on a reference flight. The hydrogen boost pump speed transient was determined for the TC-1 flight. Other trends are seen in the data. However, these are not believed to be the oxygen boost pump. Discussion of data enhancement techniques is also presented. |
| File Size | 15710299 |
| Page Count | 34 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760023167 |
| Archival Resource Key | ark:/13960/t76t5fq0j |
| Language | English |
| Publisher Date | 1976-07-01 |
| Access Restriction | Open |
| Subject Keyword | Launch Vehicles And Space Vehicles Flight Tests Titan Icbm Oxygen Centaur Launch Vehicle Power Spectra Pumps Postflight Analysis Failure Analysis Spectrum Analysis Data Processing 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 |
