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Preflight transient dynamic analyses of b-52 aircraft carrying space shuttle solid rocket booster drop-test vehicle
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Schuster, L. S. Ko, W. L. |
| Copyright Year | 1984 |
| Description | This paper concerns the transient dynamic analysis of the B-52 aircraft carrying the Space Shuttle solid rocket booster drop test vehicle (SRB/DTV). The NASA structural analysis (NASTRAN) finite element computer program was used in the analysis. The B-52 operating conditions considered for analysis were (1) landing and (2) braking on aborted takeoff runs. The transient loads for the B-52 pylon front and rear hooks were calculated. The results can be used to establish the safe maneuver envelopes for the B-52 carrying the SRB/DTV in landings and brakings. |
| File Size | 706838 |
| Page Count | 24 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840007520 |
| Archival Resource Key | ark:/13960/t85j2c88t |
| Language | English |
| Publisher Date | 1984-01-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Dynamic Structural Analysis Preflight Analysis Drop Tests Landing Gear Solid Propellant Rocket Engines Spacecraft Landing Transient Loads Nastran Space Shuttle Boosters 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 | Article |
