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Anomalous effects in dopant distribution in Ge single crystals grown by the floating zone technique aboard spacecrafts
      
Specific features of Ga-dopant distribution in Ge single crystals grown by the floating zone technique from lightly and heavily Ga-doped Ge melts aboard the Photon spacecrafts have been studied.
      
The mechanisms of the MHD effect on the properties of the grown crystals are discussed as well as the perspectives of performing analogous experiments aboard spacecrafts.
      
Computed γ-ray numbers and spectra are consistent with those of terrestrial γ-ray flashes (TGFs) observed aboard spacecrafts.
      
Experimental studies of the response of midlatitude ionospheric D region to remote launches and flights of spacecrafts using par
      
A method for simulation and optimization of flight trajectories including multiple maneuvers of spacecrafts equipped with a solar sail is considered.
      
On stability of limit cycles in stabilization systems of spacecrafts with elastic rods
      
Systems of differential motion equations perturbed by moment of external forces for spacecrafts with elastic rods and perfectly rigid bodies at their ends are constructed.
      
It has been reported that sustained arc discharge induced by electrostatic discharge (ESD) could cause permanent damage to high-power and high-voltage solar array of spacecrafts.
      
When the spacecrafts dock with each other, impact will rise at the docking point and the impact is absorbed by the docking platform.
      
Refining the outer camera orientation in synchronized shooting from two spacecrafts
      
Methods for simultaneous refining the outer orientation parameters of satellite cameras in synchronized shooting from two spacecrafts moving in the same orbit are proposed and investigated.
      
Brushless direct current motors with increased life spans for spacecrafts
      
The paper describes the dynamic performances of the electric drives of brushless motors proceeding from the dynamic performances of the flight control system used in advanced multiply spacecrafts.
      
Pulse-Width-Modulation (PWM) control strategies have been of limited interest, and use, in the regulation of a large class of mechanical systems, such as robotic manipulators and rigid spacecrafts.
      
Capillary Pumped Loop (CPL) is a thermal management device for advanced spacecrafts.
      
Space debris is very dangerous to the security of on-the-orbit spacecrafts, and it is increasing in number at high speed with the expansion of human space exploration.
      
China has sponsored the Chang' e plan of lunar exploration, and the plan along with the SMART-1 gives a good chance to lunar opposition effect research when the data on the opposition surge at very small phase angles are obtained by the spacecrafts.
      
Examples of such applications are the thermal design and modeling of spacecrafts and space-based science instruments.
      
ULF/ELF monochromatic oscillations observed by Prognoz-8 and -10 spacecrafts during quasiperpendicular supercritical shock cross
      
 

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