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Volume 25, Nº 2 (2024)
Using the principle of gravitational stabilization and orientation in the design of small spacecraft
Еsina P., Kornev V.
PDF
(Rus)
Volume 21, Nº 1 (2020)
Elaboration and testing of the algorithm which ensures an achievement of minimal deviation angle of flying model’s main centroidal axis of inertia during her counterbalancing in a sole correction flatness
Klyuchnikov A.
PDF
(Eng)
Volume 21, Nº 1 (2020)
Elaboration and testing of the algorithm which ensures an achievement of minimal deviation angle of flying model’s main centroidal axis of inertia during her counterbalancing in a sole correction flatness
Filonova M.
PDF
(Eng)
Volume 14, Nº 3 (2013)
SYNTHESIS OF THE VEHICLE ORIENTATION CONTROL SUBSYSTEM AT THE HIGH ELLIPTIC ORBIT
Yakimov E., Raevskiy V., Lukyanenko M.
PDF
(Rus)
Volume 11, Nº 7 (2010)
DYNAMIC MODELING OF A BUCKET-WHEEL EXCAVATOR PROPELLING MOTOR
Miloserdov E.
PDF
(Rus)
Volume 17, Nº 2 (2016)
NUMERICAL ALGORITHM FOR OPTIMIZATION OF A PROCESS OF CONICAL FLYING MODEL EQUILIBRATION ON A VERTICAL BALANCING STAND
Klyuchnikov A.
Volume 11, Nº 7 (2010)
MAGNETOELECTRIC EFFECT INDUCED BY ORBITAL ORDERING OF ELECTRONS
Aplesnin S., Moskvin A.
PDF
(Rus)
Volume 16, Nº 1 (2015)
The shock-absorber for executive powers of system of stabilisation of a spaceCRAFT
Vasiltsov A., Lipovtsev A.
PDF
(Rus)
Volume 11, Nº 2 (2010)
CONSTRUCTION OF DYNAMIC MODELOF RUNNING MOVER OF ROTORING DREDGE
Miloserdov E., Miloserdov E.
PDF
(Rus)
Volume 16, Nº 1 (2015)
AN ELECTROMECHANICAL EXECUTIVE BODY BASED ON THE CONTACTLESS DIRECT CURRENT MOTOR WITH A WINDING PRINTING DISK STATOR FOR SMALL SPACECRAFTS
Balandina T., Balandin E.
PDF
(Rus)
Volume 15, Nº 1 (2014)
Automated vibrating sample magnetometer with Puzey electromagnet
Velikanov D.
PDF
(Rus)
Volume 10, Nº 4 (2009)
ON CALCULATION OF MOMENT OF RESISTANCE IN CANALS OF LOW-RATE CENTRIFUGAL PUMPS
Kraeva E.
PDF
(Rus)
Volume 14, Nº 4 (2013)
THE QUESTIONS OF TECHNICAL REALIZATION OF THE DYNAMIC BENCH FOR THE RESEARCH OF THE ACTIVITY OF THE ENGINE-FLYWHEEL OF THE ATTITUDE CONTROL SYSTEM AND SPACE VEHICLE STABILIZATION
Sinitskiy D., Murigin A.
PDF
(Rus)
Volume 13, Nº 5 (2012)
EXPERIMENTAL INVESTIGATIONS OF INCOMPRESSIBLE VISCOUS FLUID IN THE FRONT GAP BETWEEN ROTATING DISK AND FIXED BOUNDARY
Zhuykov D., Falkov V., Kishkin A., Zuev A., Nazarov V.
PDF
(Rus)
Volume 13, Nº 2 (2012)
TO DYNAMIC ANALYSIS OF STEADY MOTION OF AN OUTPUT ELEMENT IN WAVE RACK AND PINION DRIVE
Limarenko G., Shevchugov M., Schepin A.
PDF
(Rus)
Volume 14, Nº 2 (2013)
ANALYSIS OF THE DYNAMIC PERFORMANCE OF THE POINTING AND ATTITUDE CONTROL SUBSYSTEM OF THE RESILIENT SPACECRAFT WITH POWER GYROSCOPIC UNIT ON THE BASIS OF ГД 02-150 GYRODYNE
Yakimov E., Raevskiy V., Lukyanenko M.
PDF
(Rus)
Volume 13, Nº 3 (2012)
THEORETICAL JUSTIFICATION OF ALGORITHM OF DETERMINATION OF AIRCRAFT ROTATING MASS MOMENTS
Ushakov N.
PDF
(Rus)
Volume 17, Nº 3 (2016)
DETERMINATION OF DYNAMIC PARAMETERS OF THE DRIVE OF THE EXPERIMENTAL STAND FOR RESEARCH OF CARDAN TRANSFERS
Struchkov A., Kukushkin E., Eresko S., Eresko T.
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