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Aerodynamic characteristics of an ogee-wing space shuttle orbiter concept at a mach number of 2.01
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Putnam, L. E. |
| Copyright Year | 1972 |
| Description | An investigation has been made at a Mach number of 2.01 to determine the effects of a flared rudder on the aerodynamic characteristics of an ogee-wing space-shuttle orbiter configuration. Also investigated were the effects of an upper-aft fuselage fairing for the orbital maneuvering system, elevon deflections, and rudder deflection on the aerodynamic characteristics of the configuration. |
| File Size | 3091966 |
| Page Count | 33 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19720010271 |
| Archival Resource Key | ark:/13960/t26b1wt9w |
| Language | English |
| Publisher Date | 1972-02-01 |
| Access Restriction | Open |
| Subject Keyword | Space Vehicles Variable Sweep Wings Space Shuttles Control Surfaces Fuselages Aerodynamic Characteristics Spacecraft Configurations Space Stations Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |