Probe design and system integration

Details Probe design and system integration Probe design and system integration

Aug 1974

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1974oppt.works....c&link_type=abstract

In Dynatrend, Inc. Proc. of Outer Planet Probe Technol. Workshop, Sect. 1 through 11 11 p (SEE N75-20358 12-12)

Physics

Equipment Specifications, Saturn (Planet), Space Probes, Uranus (Planet), Feasibility Analysis, Heat Shielding, Outer Planets Explorers, Planetary Atmospheres

Scientific paper

The feasibility of a common Saturn Uranus probe design is studied by considering the extreme atmospheres of both planets and their effects on a Pioneer spacecraft. It seems that approximately 85 percent of existing hardware can be used in an Uranus probe design, assuming that the design entry g level is somewhat reduced from current requirements. Additional development efforts include heat shielding, remotely activated batteries, mass spectrometer optimization, thermal insulation materials and high g packaging concepts.

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