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Orbiter landing loads math model description and correlation with alt flight data
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Schliesing, J. A. Hamilton, D. A. Zupp Jr., G. A. |
| Copyright Year | 1980 |
| Description | Results of the space shuttle approach and landing test are examined in order to assess landing gear characteristics and performance and verify landing dynamic analyses. The landing gears were instrumented with load-calibrated strain gages, a wheel-speed sensor, and strut stroke measurement devices. The mathematical procedure used in predicting the shuttle touchdown loads and dynamics is presented together with the comparisons between measured flight data and the analytical predictions. Conclusions from these data are also presented. |
| File Size | 13143355 |
| Page Count | 30 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800007831 |
| Archival Resource Key | ark:/13960/t8vb2z97z |
| Language | English |
| Publisher Date | 1980-01-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance Approach and Landing Tests Sts Landing Gear Performance Prediction Spacecraft Landing Mathematical Models Impact Loads Space Shuttle Orbiters 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 |
