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Solid propellant rocket motor and method of making same
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Thibodaux Jr., J. G. |
| Copyright Year | 1977 |
| Description | A method is described for making a solid propellant rocket motor having a specific concavity formed within the fuel charge. A mandrel with an aperature wider than that of the casing is inserted within the motor casing and a solidifiable propellant cast above the mandrel. The mandrel is removed after the propellant is cured. |
| File Size | 574986 |
| Page Count | 6 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19770010200 |
| Archival Resource Key | ark:/13960/t1qg3h52z |
| Language | English |
| Publisher Date | 1977-01-04 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Rocket Engine Cases Solid Propellant Rocket Engines Propulsive Efficiency Propellant Casting Propulsion System Performance Solid Rocket Propellants Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Patent |
