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Investigation of effect of propulsion system installation and operation on aerodynamics of an airbreathing hypersonic airplane at mach 0.3 to 1.2
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Mercer, C. E. Cubbage, J. M. |
| Copyright Year | 1977 |
| Description | Results from an investigation of the effects of the operation of a combined turbojet/scramjet propulsion system on the longitudinal aerodynamic characteristics of a 1/60-scale hypersonic airbreathing launch vehicle configuration are presented. Decomposition products of hydrogen peroxide were used for simulation of the propulsion system exhaust. |
| File Size | 6449870 |
| Page Count | 95 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19770021149 |
| Archival Resource Key | ark:/13960/t29931c92 |
| Language | English |
| Publisher Date | 1977-07-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Wind Tunnel Tests Aerodynamic Configurations Launch Vehicles Aerodynamic Characteristics Supersonic Combustion Ramjet Engines Hypersonic Vehicles Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |