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Design and Fabrication of the ISTAR Direct-Connect Combustor Experiment at the NASA Hypersonic Tunnel Facility

Design and Fabrication of the ISTAR Direct-Connect Combustor Experiment at the NASA Hypersonic Tunnel Facility

          
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About the Book

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. Lee, Jin-Ho and Krivanek, Thomas M. Glenn Research Center NASA/TM-2005-213432, AIAA Paper 2005-0611, E-14966 WBS 22-794-50-20 ROCKET-BASED COMBINED-CYCLE ENGINES; SYSTEMS INTEGRATION; FULL SCALE TESTS; WIND TUNNEL TESTS; COMBUSTION CHAMBERS; HYDROCARBON FUELS; EXPERIMENT DESIGN; SUPERSONIC COMBUSTION RAMJET ENGINES; FLAME PROPAGATION; COMBUSTION PHYSICS; HYPERSONIC COMBUSTION; HYDROCARBON COMBUSTION; COMBUSTION STABILITY


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Product Details
  • ISBN-13: 9798669959104
  • Publisher: Independently Published
  • Publisher Imprint: Independently Published
  • Height: 280 mm
  • No of Pages: 24
  • Spine Width: 1 mm
  • Width: 216 mm
  • ISBN-10: 8669959100
  • Publisher Date: 28 Jul 2020
  • Binding: Paperback
  • Language: English
  • Returnable: N
  • Weight: 82 gr


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Design and Fabrication of the ISTAR Direct-Connect Combustor Experiment at the NASA Hypersonic Tunnel Facility
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