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Dynamic control of srb thrust tailoff for separation
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Webb, W. W. |
| Copyright Year | 1976 |
| Description | The use of the difference in chamber pressure between solid rocket booster engines as a controlling signal to the flight control system during booster thrust tailoff was examined. In addition, the control capability of the Generalized Attitude Control System (GACS) was compared to that of the baseline. Results indicate that the difference in chamber pressure signal provided essentially no improvement. However, the GACS is considerably better than the baseline in controlling during tailoff disturbances. |
| File Size | 1324618 |
| Page Count | 34 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760019161 |
| Archival Resource Key | ark:/13960/t7tn20r7q |
| Language | English |
| Publisher Date | 1976-06-15 |
| Access Restriction | Open |
| Subject Keyword | Astrodynamics Stage Separation Attitude Control Thrust Chamber Pressure Solid Propellant Rocket Engines Thrust Augmentation Thrust Control Flight Control Booster Rocket Engines Space Shuttle Boosters 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 |
