Investigation of the descent of probes with lift-drag ratio in the Jupiter atmosphere

Details Investigation of the descent of probes with lift-drag ratio in the Jupiter atmosphere Investigation of the descent of probes with lift-drag ratio in the Jupiter atmosphere

Mar 1987

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1987kosis..25..193l&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 25, Mar.-Apr. 1987, p. 193-203. In Russian.

Physics

Descent, Gliding, Jupiter Atmosphere, Lift Drag Ratio, Space Probes, Spacecraft Control, Structural Weight, Thermal Protection, Thin Films

Scientific paper

Consideration is given to the descent of probes with low and high lift-drag ratios (LDRs) in the Jupiter atmosphere. The flight of a gliding probe with high LDR is considered in terms of the approximate selection of descent modes according to the minimum-weight criterion of the thermal-protection coating. An analysis is made of the feasibility of creating a program for the control of low LDRs by the removal of an additional film on the protective coating and for invariant turn-angle control for assuring the maximum relative weight of a segmented-conical probe.

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