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Pioneer Venus probe models instrumented prop testsModels of both the small and large Pioneer Venus probes were dropped from a helicopter to simulate the conditions of Mach and Reynolds numbers to be encountered by the probes upon entry into the Venus atmosphere. The models were dropped at an average Mach number of .10 and at an average Reynolds number of 2.84 million for the small probe and 2.90 million for the large probe. After the large amplitude launching oscillations were damped, the small probe oscillations in angle of attack and in sideslip were generally less than 2 degrees. The large probe oscillations were generally less than 10 degrees. Both exhibited distinct frequencies. The motion of the small probe in a place perpendicular to the z axis was random while the large probe rotated (corkscrewed) at 1.1 cycles per second about the z axis. The average drag coefficients of the probe models were .714 for the small probe and .663 for the large probe.
Document ID
19810014641
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Muirhead, V. U.
(Kansas Univ. Lawrence, KS, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1978
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
NASA-CR-164298
KU-FRL-333-1
Report Number: NASA-CR-164298
Report Number: KU-FRL-333-1
Accession Number
81N23174
Funding Number(s)
CONTRACT_GRANT: NAS2-9414
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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