| タイトル | Design and Fabrication of the ISTAR Direct-Connect Combustor Experiment at the NASA Hypersonic Tunnel Facility |
| 本文（外部サイト） | http://hdl.handle.net/2060/20050080753 |
| 著者（英） | Krivanek, Thomas M.; Lee, Jin-Ho |
| 著者所属（英） | NASA Glenn Research Center |
| 発行日 | 2005-02-01 |
| 言語 | eng |
| 内容記述 | The Integrated Systems Test of an Airbreathing Rocket (ISTAR) project was a flight demonstration project initiated to advance the state of the art in Rocket Based Combined Cycle (RBCC) propulsion development. The primary objective of the ISTAR project was to develop a reusable air breathing vehicle and enabling technologies. This concept incorporated a RBCC propulsion system to enable the vehicle to be air dropped at Mach 0.7 and accelerated up to Mach 7 flight culminating in a demonstration of hydrocarbon scramjet operation. A series of component experiments was planned to reduce the level of risk and to advance the technology base. This paper summarizes the status of a full scale direct connect combustor experiment with heated endothermic hydrocarbon fuels. This is the first use of the NASA GRC Hypersonic Tunnel facility to support a direct-connect test. The technical and mechanical challenges involved with adapting this facility, previously used only in the free-jet configuration, for use in direct connect mode will be also described. |
| NASA分類 | Aircraft Propulsion and Power |
| レポートNO | NASA/TM-2005-213432
E-14966
AIAA Paper 2005-0611 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/220594 |
