Characteristics of electrical jet engine of Hall- type for correction of mi-crosatellites or-bits
Journal Title: Технічна механіка, Техническая механика, Technical Mechanics - Year 2014, Vol 1, Issue 1
Abstract
The research aim is to define the degree of influence of the discharge voltage on thrust performance and power characteristics of the ITM-31 Hall low-powered engine developed at the Institute of Technical Mechanics of the National Academy of Sciences of Ukraine and State Space Agency of Ukraine. Control characteristics in a power range of 18-304 W are presented. The evaluation of an allowable operating range of the discharge voltage is pioneered. The practical importance is to increase the efficiency of the Hall engine for minimizing the power consumption.
Authors and Affiliations
S. Kulagin
Keywords
Related Articles
- EP ID EP357382
- DOI -
- Views 91
- Downloads 0
Simulation of the evolution of a droplet cloud thrown into the atmosphere as a result of an explosion of a launch vehicle with self-inflammable propellant components
The aim of this work is to develop a methodological approach to simulating the evolution of a droplet cloud (DC) formed as a result of an explosion of a launch vehicle with self-inflammable propellant components in the i...
Numerical studies in effects of 3d location of high-speed vehicle related to track structure on aerodynamic characteristics
The flow around high-speed vehicle near the track structure was calculated using the three-dimensional Reynolds averaged Navier–Stokes equations. For the turbulence simulation the SST model was used. The finite volume me...
Experimental Investigations of Multiblade Wind Wheel Model
The majority of the existing techniques for studying the characteristics of physical models of wind genera-tors are oriented on the use of the specialized equipment and a wind tunnel. In some cases, these investigations...
Classification of aerodynamic systems for low Earth orbit space hardware deorbiting
The aim of this paper is to develop a classifier of aerodynamic systems for low Earth orbit space hardware deorbiting. Aerodynamic deorbiting systems are classified. A coding scheme for systems of this type is proposed....
Active flight control for launch vehicle; a new approach and rational ways for its realization
To provide a safe operation of a launch vehicle (LV) and to use effectively its onboard service life, the ra-tional ways for forming the algorithm for an active flight control are examined based on the LV status monitori...