Multi-frequency doppler radio sounding of the ionosphere in the “Equatorial trigger” experiment

Results of processing the data of multi-frequency Doppler sounding of the low-latitude ionosphere are presented. Interesting features in the behavior of time variations of the Doppler frequency shift are found. These features are interpreted as manifestations of wave disturbances in the ionospheric plasma density.     

Numerical simulation of gas dynamics and heat exchange of jet impinging on a surface

The results of verification calculation of single jets impinging on a pedestal are presented; the result of calculations is evaluation of the local Nusselt numbers and flow gas-dynamic characteristics. On the basis of literature analysis we picked out several turbulence models to close the system of equations. The calculation results are compared with the known experimental data. It is shown, that only the v ² ? f turbulence model allows the augmented turbulence characteristics to be predicted adequately that correspond to a change of the flow conditions at short jet-to-surface distances. All models being investigated except the Spalart-Allmaras model show satisfactory agreement both in the stagnation region and in the near-wall jet zone.     

Uncontrolled Attitude Motion of the Foton-12 Satellite and Quasi-Steady Microaccelerations onboard It

The results of determination of the uncontrolled attitude motion of the Foton-12 satellite (placed in orbit on September 9, 1999, terminated its flight on September 24, 1999) are presented. The determination was carried out by the onboard measurement data of the Earth's magnetic field strength vector. Intervals with a duration of several hours were selected from data covering almost the entire flight. On each such interval the data were processed simultaneously using the least squares method by integrating the satellite's equations of motion with respect to the center of mass. The initial conditions of motion and the parameters of the mathematical model employed were estimated in processing. The results obtained provided for a complete representation of the satellite's motion during the flight. This motion, beginning with a small angular velocity, gradually sped up. The growth of the component of the angular velocity with respect to the longitudinal axis of the satellite was particularly strong. During the first several days of the flight this component increased virtually after every passage through the orbit's perigee. As the satellite's angular velocity increased, its motion became more and more similar to the regular Euler precession of an axisymmetric rigid body. In the last several days of flight the satellite's angular velocity with respect to its longitudinal axis was about 1 deg/s and the projection of the angular velocity onto the plane perpendicular to this axis had a magnitude of approximately 0.15 deg/s. The deviation of the longitudinal axis from the normal to the orbit plane did not exceed 60°. The knowledge of the attitude motion of the satellite allowed us to determine the quasi-steady microacceleration component onboard it at the locations of the technological and scientific equipment.     

Micromechanical gyros & accelerometers for digital navigation & control systems

There is no general consensus of opinion about the future of micromechanical gyroscopes and accelerometers. According to the pessimistic estimation, micromechanical gyroscopes and accelerometers have attained the limit of their accuracy. However, optimists believe that micromechamical gyroscopes will soon occupy the niche of fiber-optical gyroscopes and the latter will press laser gyroscopes. The present-day development of micromechanical gyroscopes and accelerometers is aimed at improving the basic and minor parameters: sensitivity, bias, offset, drift, resolution, scale factor, and its non-linearity. High level of performance is provided by application of high technology. This is devoted to the development and manufacturing of "silicon-glass" micromechanical sensors of encapsulated-type with digital output processing. The key technological processes allowing production of micromechanical encapsulated sensors with vacuum insides are considered and the features of their design are described. The methods for maintaining high reliability of encapsulated micromechanical gyroscopes with inner getter structure are discussed. ASIC designs for control and processing of micromechanical sensor outputs allow their accuracy, which is part of modern integrated systems, to be considerably improved. Also considered are various assemblies and packaging of the ASIC and micromechanical sensor as a single product.     

Passive ionosonde operation algorithm and technique for evaluating high-frequency band communication quality

An algorithm for operation of a new software-hardware complex to be meant for evaluating the information and technical characteristics of the bandlimited communication systems operating in the high-frequency band is presented. The algorithm makes it possible to evaluate jamresistant radio-channels in the aeronautical, marine, and other long-range radio links using the data on their passive oblique sounding by linear FM signals.     

Microflora in the basal strata at Antarctic ice core above the Vostok lake.

The microbiological investigations of the Antarctic ice core at the Vostok station become especially important in connection with the discovery of an subglacial lake in this region. This lake is considered by the world-wide scientific community to be an important object for searching for relict forms of life on the Earth and also as a model for solving a number of problems of exobiology--for instance for development of methods to penetrate into underice sea at Europe--Jupiter's satellite. For the first time the Antarctic ice core samples were taken from the horizons which correspond to the basal zone (3534-3541 m) and to the accreation ice zone (3555-3611 m) above the subglacial lake Vostok. As a result of the microbiological investigations it was shown that the total number of microbial cells have been in the same range of quantities as at the upper, younger horizons and varied from 1.3 x 10(2) up to 9.6 x 10(2) cl/ml. Some periodicity in the cell concentration and in their morphological diversity was revealed along the core. The maximal number and the greatest morphological variety were detected at horizons with the depth of 3534, 3555 and 3595 m. A drop in the cell concentration two or three times as much was found in ice layers under each of the above mentioned horizons. The discovered stratification is apparently connected with the periodicity of the lake water interactions with the basal ice layer and obviously depends on the complex natural events which took place in the geological history of our planet.     

Gasodynamic igniter with an annular nozzle

The results of numerical simulation of a flow in the complex-shaped channels and experimental investigation of characteristics of a gasodynamic igniter equipped with a plug nozzle are presented. It is shown that the igniter characteristics are significantly improved as a result of replacing an acoustic nozzle by an annular one.     

Mars/Moon Cratering Rate Ratio Estimates

This article presents a method to adapt the lunar production function, i.e. the frequency of impacts with a given size of a formed crater as discussed by Neukum et al. (2001), to Mars. This requires to study the nature of crater-forming projectiles, the impact rate difference, and the scaling laws for the impact crater formation. These old-standing questions are reviewed, and examples for the re-calculation of the production function from the moon to Mars are given.     

A Study of Rayed Structures in Auroras by Triangulation Methods: 1. Height Profiles of Volume Emission Rate

Cosmic Research - A technique is presented for reconstructing the height profiles of the volume emission rate and estimating the crosscut dimensions of rayed structures in auroras from the data of...     

Physicochemical model of the auroral ionosphere

A physicochemical model of excited polar ionosphere has been presented. The model makes it possible to calculate vertical profiles of concentrations of the following excited and ionized constituents: O₂ ⁺, N₂ ⁺, O⁺(⁴S), O⁺(²D), O⁺(²P), O(¹D), O(¹S), N(⁴S), N(²D), N(²P), NO, NO⁺, N⁺, N₂(A³Σ_u ⁺), N₂(B³П_g), N₂(W³Δ_u), and N₂(B′³Σ_u ^-) and the electron concentration during electron precipitations. The energy spectrum of the electrons at the upper boundary of the ionosphere and concentrations of neutral constituents are the input parameters of the model. A model has been compiled based on available publications and includes 56 physicochemical reactions that influence concentrations of the aforementioned constituents in the polar ionosphere. The method of calculating vertical profiles of the excitation rates of atmospheric gases and proper allowance for the electron-vibrational kinetics in the processes of exciting the triplet states of N₂ are specific features of the presented model. The ionospheric model has been approbated using the results of the coordinated rocket–satellite experiment. The agreement between the modeling results and experimental data best for the time being is achieved.