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Debris control design achievements of the booster separation motors
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Chase, C. A. Smith, G. W. |
| Copyright Year | 1985 |
| Description | The stringent debris control requirements imposed on the design of the Space Shuttle booster separation motor are described along with the verification program implemented to ensure compliance with debris control objectives. The principal areas emphasized in the design and development of the Booster Separation Motor (BSM) relative to debris control were the propellant formulation and nozzle closures which protect the motors from aerodynamic heating and moisture. A description of the motor design requirements, the propellant formulation and verification program, and the nozzle closures design and verification are presented. |
| File Size | 813019 |
| Page Count | 11 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19850008633 |
| Archival Resource Key | ark:/13960/t3227sh4r |
| Language | English |
| Publisher Date | 1985-01-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Stage Separation Insulation Damage Assessment External Tanks Constraints Thermal Protection Space Shuttle Main Engine Structural Design Criteria Space Shuttle Ascent Stage Debris Space Shuttle Orbiters Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
