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Dynamic assessment of b-52b-008 carrier aircraft for the revised space shuttle solid rocket booster decelerator subsystem drop test vehicle
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Doty, L. J. |
| Copyright Year | 1983 |
| Description | The structural integrity of B-52B-008, pylon, and hooks for the drop test missions was determined by theoretical analysis. The results of the analysis and conclusions are presented in this document. The major modification to the drop test vehicle was shortening it about 54 inches, which resulted in the forward hook attach structure being located at the base of the nosecone. The shims that are located in the aft hook structures are increased from two inches to three inches. Airspeed, aerodynamic configuration, and load charts are included. |
| File Size | 33646604 |
| Page Count | 54 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840013538 |
| Archival Resource Key | ark:/13960/t1rg0k98n |
| Language | English |
| Publisher Date | 1983-12-16 |
| Access Restriction | Open |
| Subject Keyword | Space Transportation Performance Tests Subsonic Flutter Structural Stability Aircraft Instruments Data Processing Fuel Consumption Dynamic Loads Systems Integration Space Shuttle Boosters Pylons Aerodynamic Configurations Drop Tests Parachute Descent Hooks Test Equipment Aerodynamic Characteristics Structural Analysis B-52 Aircraft 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 |
