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Equations for calculating orbiter surface erosion and breakage rates in ius and ssus srm exhaust plumes
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Wilson, S. W. |
| Copyright Year | 1978 |
| Description | Equations and coefficients for calculating the flux of solid particles in the exhaust plumes of the interim upper stage and SSUS solid rocket motors (SRM) are considered. Modifications required to account for the independent motions of the orbiter and the SRM, such as will result during an on-orbit SRM firing are described. |
| File Size | 5671033 |
| Page Count | 36 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19780019230 |
| Archival Resource Key | ark:/13960/t7fr4pg4b |
| Language | English |
| Publisher Date | 1978-06-06 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Particle Size Distribution Algorithms Surface Reactions Exhaust Gases Inertial Upper Stage Solid Propellant Rocket Engines Upper Stage Rocket Engines Mathematical Models Space Shuttle Orbiters Impact Damage Erosion 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 |
