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Space shuttle plume/simulation application
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Conine, B. Boyle, W. Bell, G. |
| Copyright Year | 1979 |
| Description | An analysis of pressure and strain-gage data from space shuttle wind tunnel test IA119 and IA138 was performed to define the influence on aerodynamic characteristics resulting from the main propulsion system and solid rocket booster plumes. Aerodynamic characteristics of each of the elements, the components and total vehicle of the space shuttle vehicle during ascent flight was considered. Pressure data were obtained over the aft portions of the space shuttle wind tunnel model in addition to wing and elevon gage data. |
| File Size | 2960862 |
| Page Count | 75 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19790021050 |
| Archival Resource Key | ark:/13960/t75t8ff75 |
| Language | English |
| Publisher Date | 1979-05-15 |
| Access Restriction | Open |
| Subject Keyword | Space Transportation Wings Aerodynamic Configurations Elevons Ascent Propulsion Systems Solid Rocket Propellants Space Shuttles Supersonic Wind Tunnels Wind Tunnel Tests Rocket Exhaust Pressure Aerodynamic Characteristics 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 |