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Study of solid rocket motors for a space shuttle booster. volume 4: mass properties report
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Vonderesch, A. H. |
| Copyright Year | 1972 |
| Description | Mass properties data for the 156 inch diameter, parallel burn, solid propellant rocket engine for the space shuttle booster are presented. Design ground rules and assumptions applicable to generation of the mass properties data are described, together with pertinent data sources. |
| File Size | 178188 |
| Page Count | 9 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19720015130 |
| Archival Resource Key | ark:/13960/t11p2vg33 |
| Language | English |
| Publisher Date | 1972-03-15 |
| Access Restriction | Open |
| Subject Keyword | Propulsion Systems Solid Propellant Rocket Engines Propulsion System Performance Propulsion System Configurations Systems Engineering Space Shuttle Boosters Mass Flow 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 |
