Telemetry information registration, processing and control 1Makarov AL, 2Khrapach AV. Telemetry information registration, processing and control. Kosm. nauka tehnol. 2002 ;8(Supplement1):088-090.
Method of multipole analyzes for determination of planet's magnetic moments 1Degtiariov VV, 1Degtiariov AV. Method of multipole analyzes for determination of planet's magnetic moments. Kosm. nauka tehnol. 2002 ;8(Supplement1):085-088.
Conception to arrange of regional system for reception, obtaining and processing DSE data 1Bogomia VV, 1Zagorulko AN, 1Malevinskii SV, 1Mironenko VN. Conception to arrange of regional system for reception, obtaining and processing DSE data. Kosm. nauka tehnol. 2002 ;8(Supplement1):080-084.
Increase of reliability of information receiving in satellite communication systems at specified speed of its transmission 1Bobrov AI, 1Bobrov SI. Increase of reliability of information receiving in satellite communication systems at specified speed of its transmission. Kosm. nauka tehnol. 2002 ;8(Supplement1):077-079.
Investigation and method development of quality estimate of catalogues of space object motion parameters 1Brovko MV, 1Golubek AV, 1Emelianova IA, 1Khorolskyi PG. Investigation and method development of quality estimate of catalogues of space object motion parameters. Kosm. nauka tehnol. 2002 ;8(Supplement1):073-077.
On a new method of geostationary satellites drift compensation 1Paltsev NG. On a new method of geostationary satellites drift compensation. Kosm. nauka tehnol. 2001 ;7(Supplement1):102-103.
Reusable transport space systems with application of air launch 1Sokol AV, 1Popov VA, 2Poluian MV. Reusable transport space systems with application of air launch. Kosm. nauka tehnol. 2001 ;7(Supplement1):100-102.
Behaviour of spacecrafts group injecting by one laungh vehicle 1Paltsev NG. Behaviour of spacecrafts group injecting by one laungh vehicle. Kosm. nauka tehnol. 2001 ;7(Supplement1):097-100.
Experimental verification of possibility of spacecraft initial orbit determination using radial velocity measured by one measuring point 1Sheptun AD, 2Ivanov OM, 2Mashtak IV. Experimental verification of possibility of spacecraft initial orbit determination using radial velocity measured by one measuring point. Kosm. nauka tehnol. 2001 ;7(Supplement1):092-097.
Method of determination of aerodynamic axial force acting on vehicle body and stabilizer on it 1Ermolenko EA, 1Kamenchuk Yu.V. Method of determination of aerodynamic axial force acting on vehicle body and stabilizer on it. Kosm. nauka tehnol. 2001 ;7(Supplement1):089-092.