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Ballistics/mass properties
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Drendel, Albert S. Richards, M. C. |
| Copyright Year | 1989 |
| Description | The propulsion performance and reconstructed mass properties data from Morton Thiokol's RSRM-4 motors, which were assigned to the STS-30R launch, are presented. The composite type solid propellant burn rates were close to predicted. The performance of the pair of motors were compared to some CEI Specification CPW1-3600 for compliance. Some aspects of the CEI Specification could not be compared because of low sampling of data. The performance of the motors were well within the CEI specification requirements. Post flight reconstructured RSRM mass properties are within expected values for the RSRM quarterweight and halfweight configurations. |
| File Size | 962760 |
| Page Count | 39 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19900003336 |
| Archival Resource Key | ark:/13960/t19k97m1k |
| Language | English |
| Publisher Date | 1989-06-23 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Grain Size Composite Propellants Propulsion System Performance Propellant Grains Solid Propellant Rocket Engines Propulsive Efficiency Ballistics Engine Tests Rocket Engine Design Burning Rate 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 |
