No. 2 (2026): Technical Mechanics

Published: 2026-07-02

Aviation and Space Engineering

FEATURES OF THE AERODYNAMIC OPTIMIZATION OF THE SPATIAL SHAPE OF AXIAL-FLOW COMPRESSOR BLADES

Yu. O. KVASHA, N. A. ZINEVYCH, N. V. PETRUSHENKO

3-9
AEROSTATIC SYSTEMS IN DEFENSE APPLICATIONS: THE CURRENT CHALLENGES AND THE STATE OF THE ART

V. K. SHAMAKHANOV, B. I. TEROKHIN, E. O. LAPKHANOV

10-22
DEPLOYMENT OF THE ROTATING TWO BODIES TETHER IN AN ORBIT

Ch. WANG, O. E. ZAKRZHEVSKYI

23-37
ANALYSIS OF THE MAGNETIC FIELD AND THE MAGNETIC FLUX IN SPACECRAFT’S PASSIVE DEORBIT SYSTEMS

B. V. YURKOV, S. Yu. ASMOLOVSKYI, S. M. KULAHIN, M. P. RIZNYCHENKO

38-48
ELECTROJET THRUSTER TO BALANCE AN AERODYNAMIC DRAG ON A SMALL SPACECRAFT IN A VERY LOW EARTH ORBIT

O. D. GRYSHKEVYCH

49-61
PROSPECTS FOR THE IMPLEMENTATION OF ERP SYSTEMS AND MODULAR ARCHITECTURE IN SPACE ENTERPRISE MANAGEMENT

I. O. HUSAROVA, D. V. KLYMENKO

62-68
DEVELOPMENT AND CHARACTERIZATION OF A METAL PLASMA VACUUM-ARC THRUSTER

Ye. V. SPIRIN

69-78
EFFECT OF THE TEMPERATURE ON THE PARAMETERS OF CAPILLARY PROPELLANT MANAGEMENT DEVICES

S.O. DAVYDOV, M.O. KATRENKO, N.S. PRYADKO

79-87

Applied Mechanics

ANALYSIS OF THE STRAIN OF A SUBSOILER CHAIN LINK AND ITS FORMING BEHAVIOR UNDER STATIC LOADING

B. A. SHELUDCHENKO, Ye. S. SYROID

88-97
MATHEMATICAL SIMULATION OF THE STRESS AND STRAIN FIELD OF HIP JOINT ELEMENTS UNDER STATIC LOADS AT DIFFERENT STAGES AFTER A TOTAL HIP ARTHROPLASTY

D. V. HOROBETS, M. B. SOBOLEVSKA, O. Ye. LOSKUTOV

98-110