Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Walter E. Bruce"'
Publikováno v:
J Thermophys Heat Trans
The Hypersonic Materials Environmental Test System arc-jet facility located at the NASA Langley Research Center in Hampton, Virginia, is primarily used for the research, development, and evaluation of high-temperature thermal protection systems for h
Publikováno v:
Journal of Spacecraft and Rockets. 51:789-800
A methodology to correlate flight aeroheating environments to the arc-jet environment is presented. For a desired hot-wall flight heating rate, the methodology provides the arc-jet bulk enthalpy for the corresponding cold-wall heating rate. A series
Autor:
Walter E. Bruce, Melissa B. Carter, Alaa A. Elmiligui, Courtney S. Winski, Sudheer Nayani, Raymond S. Castner
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
Autor:
Melissa B. Carter, Alaa A. Elmiligui, Sudheer N. Nayani, Raymond S. Castner, Walter E. Bruce, Jacob Inskeep
Publikováno v:
53rd AIAA Aerospace Sciences Meeting.
NASA has been conducting research into reducing sonic boom and changing FAA regulations to allow for supersonic commercial transport over land in the United States. This particular study looks at a plume passing through a shock generated from an aft
Publikováno v:
AIAA Ground Testing Conference.
A methodology to correlate flight aeroheating environments to the arc-jet environment is presented. For a desired hot-wall flight heating rate, the methodology provides the arcjet bulk enthalpy for the corresponding cold-wall heating rate. A series o
Autor:
Stephen J. Hughes, Joseph A. DelCorso, Anthony M. Calomino, Walter E. Bruce, F. McNeil Cheatwood
Publikováno v:
21st AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar.
Typical entry vehicle aeroshells are limited in size by the launch vehicle shroud. Inflatable aerodynamic decelerators allow larger aeroshell diameters for entry vehicles because they are not constrained to the launch vehicle shroud diameter. During
Publikováno v:
20th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar.
The Program to Advance Inflatable-Decelerators for Atmospheric Entry (PAIDAE) is a NASA project tasked with developing and evaluating viable inflatable-decelerator aeroshell geometries and materials. Thermal analysis of material layups supporting an
Publikováno v:
AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference.
The Hyper -X (X -43A) program’s goal was to conduct flight experiments demonstrating scramjet performance and operability under controlled powered free -flight conditions at Mach 7 and 10. The Mach 7 and Mach 10 flights were successfully completed
Conference
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