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Solid rocket booster performance evaluation model. volume 3: sample case. [propellant combustion simulation/internal ballistics
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1974 |
| Description | The solid rocket booster performance evaluation model (SRB-11) is used to predict internal ballistics in a sample motor. This motor contains a five segmented grain. The first segment has a 14 pointed star configuration with a web which wraps partially around the forward dome. The other segments are circular in cross-section and are tapered along the interior burning surface. Two of the segments are inhibited on the forward face. The nozzle is not assumed to be submerged. The performance prediction is broken into two simulation parts: the delivered end item specific impulse and the propellant properties which are required as inputs for the internal ballistics module are determined; and the internal ballistics for the entire burn duration of the motor are simulated. |
| File Size | 15095587 |
| Page Count | 269 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19770020239 |
| Archival Resource Key | ark:/13960/t6741jj05 |
| Language | English |
| Publisher Date | 1974-09-07 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Propulsion System Performance Solid Propellant Rocket Engines Performance Prediction Electronic Modules Propulsive Efficiency Parameterization Booster Rocket Engines Propellant Combustion Space Shuttle Boosters Computer Programs 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 |
