On motion of a spacecraft with the constantly oriented solar sail
Authors: Vaskova V.S., Rodnikov A.V.
Issue: #9 (165)
Mechanics
Description of dynamics of a ring micromechanical gyroscope with the form defect based on a model of the flexible resilient curvilinear rods
Authors: Kiselev R.M., Sorokin F.D.
Aviation and Rocket-Space Engineering
Studying efficiency of the protective structures made with the corundum sand under a high-velocity ballistic impact using the modified computational and experimental method
Authors: Zuzov V.N., Yakovlev D.A., Zhurkin M.M.
A method for loading the structurally similar sample of a thick-walled composite three-span stringer panel of the wing torsion box by combined action of the compressive and shear loads
Authors: Perelomov K.A.
Studying power capabilities of a small space tugfor providing peripheral launch services in the sun-synchronous orbits
Authors: Galkin A.A., Georgiev A.F., Shcheglov G.A.
Transformable assemblies of a unified space module for the Metamorphosis transport and cargo system designed for Moon exploration
Authors: Stepashkin A.B., Nikulin I.E.
Development of methods for the design and mathematical support of an on-board technical system to maintain the efficiency of astronauts in the conditions of a habitable lunar base
Authors: Baranov M.S.
Development of the new criteria equations to compute the electrostatic field effect on intensification of heat transfer to the MS-20 motor aviation oil exposed to its forced convection
Authors: Lvov M.V., Altunin V.A., Altunin K.V.