Study of new systems concepts for a Titan atmospheric probe

Details Study of new systems concepts for a Titan atmospheric probe Study of new systems concepts for a Titan atmospheric probe

Apr 1986

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1986hair.rept.....b&link_type=abstract

Final Technical Report Hughes Aircraft Co., El Segundo, CA. Space and Communications Group.

Computer Science

Atmospheric Composition, Planetology, Space Probes, Spacecraft Design, Titan, Antenna Design, Costs, Mission Planning, Structural Design Criteria

Scientific paper

Results of a systems concepts study for a Titan Probe were examined. The key tradeoffs performed are described in detail. Mass breakdown of each Probe subsystem or major element were given. The mission analysis performed to determine compliance with the high altitude sampling and descent time requirements are described. The baseline Descent Module design was derived. The element of the Probe System left on the Carrier after separation were described.

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