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Structural load reduction of the space shuttle booster/orbiter configuration using a load relief guidance technique
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Kelley, P. B. Deaton, A. W. |
| Copyright Year | 1973 |
| Description | A space shuttle booster/orbiter atmospheric ascent guidance algorithm is developed that will reduce the aerodynamically induced structural loads as compared to an open loop guidance algorithm. |
| File Size | 1275326 |
| Page Count | 35 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19730013085 |
| Archival Resource Key | ark:/13960/t0cv98m4j |
| Language | English |
| Publisher Date | 1973-04-05 |
| Access Restriction | Open |
| Subject Keyword | Space Sciences Structural Engineering Trajectory Analysis Space Shuttles Aerodynamic Loads Ascent Trajectories 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 |