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Absorbed acoustic radiation as a factor of the transformation of inertial sensing elements of gyrostabilized platforms into impedance ones. Mixed boundary problem. Kosm. nauka tehnol. 2011 ;17(2):22-31.
. Additional errors of a gyroscopic integrator of linear launcher accelerations caused by the diffraction of sound waves. Kosm. nauka tehnol. 2001 ;7(2-3):027–032.
. On additional errors of float gyroscope during circulation of a carrier rocket. Kosm. nauka tehnol. 2009 ;15(6):49-56.
. Errors of measurements of longitudinal speeds of rocket carriers by gyroscopic integrator. Kosm. nauka tehnol. 2002 ;8(1):081-088.
. On the fault in constructing the vertical in rocket launch. Kosm. nauka tehnol. 1999 ;5(4):70–74.
. On the fault in the course indication of carrier rocket. Kosm. nauka tehnol. 1999 ;5(5):77–80.
. Generator of aerodynamic noise in ground complexes for spacecraft testing. Kosm. nauka tehnol. 1998 ;4(2):87–92.
. Hypersound breach: prospects and problems. Kosm. nauka tehnol. 2013 ;19(2):63–73.
. On the impact of acoustic radiation on the dynamics of sensitive elements in gyrostabilized platforms. Kosm. nauka tehnol. 1995 ;1(2):72–75.
. Influence of acoustinc emission on the dynamics of resilient suspenders of rocket control devices. Kosm. nauka tehnol. 1999 ;5(2):73–77.
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