A four month feasibility study of a hypersonic real-gas free flight test facility for NASA Langley Research Center (LARC) was performed. The feasibility of using a high-energy electromagnetic launcher (EML) to accelerate complex models (lifting and nonlifting) in the hypersonic, real-gas facility was examined. Issues addressed include: design and performance of the accelerator; design and performance of the power supply; design and operation of the sabot and payload during acceleration and separation; effects of high current, magnetic fields, temperature, and stress on the sabot and payload; and survivability of payload instrumentation during acceleration, flight, and soft catch
The two principal areas of advanced propulsion investigated are the ram accelerator and the flowing ...
Assessing research and development in hypersonic aircraft for determining requirements for hypersoni...
A hypersonic airbreathing missile using dual mode scramjet engines for propulsion is described. The ...
Described are the modifications currently under way to the Langley 8-Foot High Temperature Tunnel to...
The Hypersonic Tunnel Facility (HTF) at NASA Lewis Research Center's Plum Brook Station is a blowdow...
The primary objective of the workshop was to obtain a critical assessment of a concept for a large, ...
Strain gages, nitrocellulose effects, and mathematical models for hypervelocity launch tubes with pr...
Four facility activities are underway at NASA Lewis Research Center to develop new hypersonic propul...
Future aircraft may be hydrogen fueled and fly at hypersonic speeds. The resulting environments will...
Tranverse mode stability characteristics of coaxial and hyperthin injectors in tranverse excitation ...
Mechanical features of 25.4 mm light gas gun model launcher and performance data for developmental f...
A conceptual design of a very large aeroballistic range is presented, as are its operational charact...
Addition of kinetic energy to supersonic exhaust of shock tunnel by reversing flow direction with hi...
Integrating spacecraft/experiment payloads for solar-thermionic flight test vehicl
Performance study for application of Saturn V to high energy earth escape mission
The two principal areas of advanced propulsion investigated are the ram accelerator and the flowing ...
Assessing research and development in hypersonic aircraft for determining requirements for hypersoni...
A hypersonic airbreathing missile using dual mode scramjet engines for propulsion is described. The ...
Described are the modifications currently under way to the Langley 8-Foot High Temperature Tunnel to...
The Hypersonic Tunnel Facility (HTF) at NASA Lewis Research Center's Plum Brook Station is a blowdow...
The primary objective of the workshop was to obtain a critical assessment of a concept for a large, ...
Strain gages, nitrocellulose effects, and mathematical models for hypervelocity launch tubes with pr...
Four facility activities are underway at NASA Lewis Research Center to develop new hypersonic propul...
Future aircraft may be hydrogen fueled and fly at hypersonic speeds. The resulting environments will...
Tranverse mode stability characteristics of coaxial and hyperthin injectors in tranverse excitation ...
Mechanical features of 25.4 mm light gas gun model launcher and performance data for developmental f...
A conceptual design of a very large aeroballistic range is presented, as are its operational charact...
Addition of kinetic energy to supersonic exhaust of shock tunnel by reversing flow direction with hi...
Integrating spacecraft/experiment payloads for solar-thermionic flight test vehicl
Performance study for application of Saturn V to high energy earth escape mission
The two principal areas of advanced propulsion investigated are the ram accelerator and the flowing ...
Assessing research and development in hypersonic aircraft for determining requirements for hypersoni...
A hypersonic airbreathing missile using dual mode scramjet engines for propulsion is described. The ...