Development of design for 'Venera' landers

Details Development of design for 'Venera' landers Development of design for 'Venera' landers

Jul 1982

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1982rpspr.......16z&link_type=abstract

In its USSR Rept.: Space, No. 16 (JPRS-81359) p 16-17 (SEE N82-30269 20-99) Transl. into ENGLISH from Sots. Industr. (USSR), 1

Other

Aerodynamic Stability, Descent Trajectories, Soft Landing Spacecraft, Spacecraft Stability, Venera Satellites, Wind Tunnel Stability Tests, Atmospheric Turbulence, U.S.S.R. Space Program, Venus Atmosphere

Scientific paper

Stabilizing the Venera lander descent vehicle by means of a 'notched crown' or skirt is described. Helicopter drop and wind tunnel tests are reviewed. The aerodynamics of the landers, affected by soil sampling and other devices, are summarized. Descent, oscillation, and rotation parameters are reviewed in terms of strong wind and atmospheric turbulence.

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