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Jupiter entry simulation with the ANAA shock tubeAn annular arc accelerator (ANAA) shock tube has been built which produces shock velocities and pressures that simulate entry into the atmosphere of Jupiter. The ANAA driver deposits the energy of an arc discharge into a flowing gas, which then expands and cools without any delay for the opening of a diaphragm. A flow transducer, trigger system, and spark gap switches have been developed to coordinate the flow from a high-pressure helium driver with the discharge from a 300-kJ capacitor bank. Shock velocities up to 47 km/sec have been produced in 1.0 torr of hydrogen with the ANAA shock tube, compared with 35 km/sec velocity produced in a conical arc driver with three times the available energy. Attenuation with the ANAA shock tube is comparable to that of a conical arc driver shock tube, and initial spectroscopic measurements indicate that an impurity-free test slug is formed behind the shock wave.
Document ID
19740052631
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Leibowitz, L. P.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Date Acquired
August 7, 2013
Publication Date
July 1, 1974
Subject Category
Facilities, Research, And Support
Report/Patent Number
AIAA PAPER 74-610
Meeting Information
Meeting: Aerodynamic Testing Conference
Location: Bethesda, MD
Start Date: July 8, 1974
End Date: July 10, 1974
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
74A35381
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Other

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