A discussion of some proposed measurement techniques for hypersonic flight and instrumentation research experimentsSensors, instrumentation, and test techniques proposed for the Hypersonic Flight Instrumentation and Research Experiment are discussed. The project is concerned with Mach 4 to 16 flight at pressure altitudes of 50,000 to 150,000 feet. The developmental instrumentation for the program includes angle-of-attack sensors, transition sensors, skin-friction sensors, particle sensors, species-concentration sensors, and temperature and heat flux sensors. Support instrumentation (required to monitor basic flight parameters and to supply data from which the performance of the developmental instruments may be evaluated) considered include surface pressure sensors, inertial instrumentation, magnetic attitude sensors, and signal conditioning and data transmission instrumentation.
Document ID
19880064681
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hellbaum, R. F. (NASA Langley Research Center Hampton, VA, United States)
Garner, H. Douglas (NASA Langley Research Center Hampton, VA, United States)