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Hybrid rocket propulsion for sounding rocket applications
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1991 |
| Description | A discussion of the H-225K hybrid rocket motor, produced by the American Rocket Company, is given. The H-225K motor is presented in terms of the following topics: (1) hybrid rocket fundamentals; (2) hybrid characteristics; and (3) hybrid advantages. |
| File Size | 233600 |
| Page Count | 9 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19920013360 |
| Archival Resource Key | ark:/13960/t3421w56t |
| Language | English |
| Publisher Date | 1991-01-01 |
| Access Restriction | Open |
| Subject Keyword | Launch Vehicles And Space Vehicles Hybrid Propellant Rocket Engines Rocket Oxidizers Hybrid Rocket Engines Solid Rocket Propellants Liquid Oxygen Hydrocarbon Fuels Rocket Engine Design Propellant Combustion Propulsion System Configurations Sounding Rockets Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
