Author/Authors :
G.F. Putin، نويسنده , , I.A. Babushkin، نويسنده , , G.P. Bogatyrev، نويسنده , , A.F. Glukhov، نويسنده , , E.A. Zilberman، نويسنده , , A.I. Ivanov، نويسنده , , M.M. Maksimova، نويسنده , , V.I. Polezhaev، نويسنده , , O.A. Bessonov، نويسنده , , S.A. Nikitin، نويسنده , , V.V. Sazonov، نويسنده ,
Abstract :
The arrangement of the apparatus “DACON” for examining buoyancy driven thermal convection caused by microgravity environment aboard a spacecraft is expounded. Experiments carried out with the sensor “DACON” on board the Orbital Station “Mir” during 25th – 28th missions in 1998 – 2000 are presented. The results of measurements of convection and evaluation of low-frequency microacceleration components in different modules and for various regimes of crew and Station activity are reported.
