Galileo Atmospheric Entry Probe System - Design, development, and testThe overall development of the Galileo Atmospheric Entry Probe System is described. The Probe will be carried to Jupiter by the Galileo Orbiter and released on an entry trajectory 150 days before entry. A complement of seven science instruments will measure the near-Jupiter radiation field and the characteristics of the Jovian atmosphere from a distance of about 5 Jupiter radii above the 1-bar level down to levels in the 10-20-bar range. Probe data are to be transmitted to earth via the Orbiter. System requirements are discussed. Probe design features and those features of the development test program peculiar to entry probes are described.
Document ID
19830035302
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Givens, J. J. (NASA Ames Research Center Moffett Field, CA, United States)
Nolte, L. J. (Hughes Aircraft Co. El Segundo, CA, United States)
Pochettino, L. R. (General Electric Co. Philadelphia, PA, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1983
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 83-0098
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting