Combined Cycle Engine (CCE) Test in 10 x 10 Supersonic Wind Tunn
The NASA Fundamental Aeronautics Hypersonics project is focused on technologies for combined cycle, air-breathing propulsions systems to enable reusable launch systems for access to space. Turbine Based Combined Cycle (TBCC) propulsion systems offer specific impulse (Isp) improvements over rocket-based propulsion systems in the subsonic takeoff and re turn mission segments and offer improved safety. The potential to realize more aircraft-like operations with expanded launch site capability and reduced system maintenance are additional benefits.
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Details
NASA ID
GRC-2011-C-01671
Date Created
January 29, 2011
Center
GRC
Media Type
image
Photographer
NASA/GRC/Quentin Schwinn
Location
NASA Glenn Research Center
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