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Nitramine propellants. [gun propellant burning rate
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Cohen, N. S. |
| Copyright Year | 1978 |
| Description | Nitramine propellants without a pressure exponent shift in the burning rate curves are prepared by matching the burning rate of a selected nitramine or combination of nitramines within 10% of burning rate of a plasticized active binder so as to smooth out the break point appearance in the burning rate curve. |
| File Size | 508359 |
| Page Count | 8 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19780023312 |
| Archival Resource Key | ark:/13960/t2f815576 |
| Language | English |
| Publisher Date | 1978-05-30 |
| Access Restriction | Open |
| Subject Keyword | Propellants And Fuels Plasticizers Propellant Binders Propellant Grains Gun Propellants Pressure Distribution Propellant Chemistry Nitramine Propellants Chemical Composition 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 | Patent |
