NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Galileo atmospheric entry probe mission descriptionThe mission goals, control parameters, and instrumentation for the Galileo entry probe are described. The goal for the probe is to penetrate the Jovian atmosphere to 10 bars, begin data gathering and transmission at about 0.1 bar, and make as many in-situ cloud measurements as possible. The probe will pass through a 16,000 K shock layer, which has led to a ratio of 5 kg of heat shield to every kg of instrumentation on the probe. An entry angle between -7.0 to -10.2 deg will be used, and possible targets with respect to declinations associated with a 1986 launch are discussed. The preentry mission phase, entry/descent sequence, and the baseline mission relay link performance are outlined. Data may be available down to 20 bars, and the probe performance will aid in design goals for subsequent Saturn and Uranus probes.
Document ID
19830038362
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Vojvodich, N. S.
(NASA Ames Research Center Moffett Field, CA, United States)
Schaupp, R. W.
(NASA Ames Research Center Galileo Probe Projects Office, Moffett Field, CA, United States)
Drean, R. J.
(NASA Ames Research Center Moffett Field; Hughes Aircraft Co., Culver City, CA, United States)
Farless, D. L.
(NASA Ames Research Center Moffett Field; California Institute of Technology, Jet Propulsion Laboratory, Pasadena, CA, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1983
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
AIAA PAPER 83-0100
Report Number: AIAA PAPER 83-0100
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting
Location: Reno, NV
Start Date: January 10, 1983
End Date: January 13, 1983
Accession Number
83A19580
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available