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Highly transparent and rugged sensor for velocity determinations of cosmic dust particlesIn order to understand the evolution of interplanetary dust, numerous dust particles have been collected and analyzed. An analysis of the composition often provides information on the particle's origin. So does its origin. Composition and orbit data complement each other and should be determined together. If the last orbit of a particle can be determined, its orbital history can often be calculated backward in time and associated with its parent body. To determine the last orbit, the velocity needs to be measured before the particle is collected. The precision required in determining the velocity components relative to the spacecraft should be 1 percent or better. A sensor for naturally charged cosmic dust particles is discussed. Two models of the sensor were tested, one with a free-falling steel ball and the other with particles accelerated to high speed. Analytic expressions of the sensor signals are presented and compared with the test results. The errors in speed and angle were estimated to be about 0.3 percent and 0.2 degrees respectively.
Document ID
19950012763
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Auer, Siegfried
(A & M Associates Lanham, MD, United States)
Vonbun, F. O.
(A & M Associates Lanham, MD, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1994
Publication Information
Publication: Lunar and Planetary Inst., Workshop on Particle Capture, Recovery and Velocity(Trajectory Measurement Technologies
Subject Category
Spacecraft Instrumentation
Accession Number
95N19178
Funding Number(s)
CONTRACT_GRANT: NAS9-18368
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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