Journal
Scientific and technical journal «Priborostroenie»
UDK629.78
Issue:6 (59)
Download PDF604 Kbyte
PROJECT OF NANOSATELLITE GROUP SEPARATION AT CLUSTER LAUNCHING FROM AN ORBITAL STAGE
Annotation
The possibility to use orbital stage of launch vehicle as a platform for the piggy back launch of either single or cluster of nanosatellites is considered. The program of the nanosatellites separation from an orbital stage is anticipated to provide a basis for the safe movement of nanosatellites after their group deployment. A special attention is given to the fact that after separation of the main payload, the orbital stage obtains the angular velocity, the value and direction of which is not known. Results of statistical analysis have allowed developing of a method of selecting the nanosatellites separation parameters (the velocity and time of separation). The separated values of the parameters ensure exclusion of the possibility of nanosatellites collision and reduce the satellites dispersion by a predetermined distance. Results of statistical modeling carried out for nanosatellites launching from carrier rocket Soyuz orbital stage are presented.
Keywords
Постоянный URL
Articles in current issue
- PERSPECTIVES OF SMALL SIZE SPACECRAFT DEVELOPMENT FOR VARIOUS PURPOSES AT JSC RUSSIAN SPACE SYSTEMS
- CONSTRUCTION OF SMALL SPACECRAFT CLUSTERS
- INVESTIGATION OF SOLAR-TERRESTRIAL CONNECTION AND NEAR-EARTH PLASMA WITH THE USE OF SMALL SPACECRAFTS
- DEVICE FOR CONSTRUCTING THE LOCAL VERTICAL FOR NANOSPACECRAFT
- THE SPECIFICS OF SPACE RESEARCH ON MICRO-SATELLITE PLATFORMS INTEGRATED INTO THE INFRASTRUCTURE OF RUSSIAN SEGMENT OF THE ISS
- CHOICE OF THE DESIGN PARAMETERS OF AERODYNAMICALLY STABILIZED NANOSATELLITE
- ELECTRICAL POWER SUBSYSTEM DESIGN FOR SAMSAT NANOSATELLITE
- STUDY OF INHOMOGENEOUS STRUCTURE OF THE IONOSPHERE USING SIMULTANEOUS MEASUREMENTS BY NANOSATELLITES OF CUBESAT STANDARD
- ANALYSIS OF POSSIBLE FAILURES OF STANDARD NANOSATELLITE
- PROSPECTS OF REALIZATION OF PROTO-FLIGHT APPROACH IN NANOSATELLITE GROUND TESTING
- SMALL SPACECRAFT LAUNCHING SYSTEM
- COMPACT AUTOMATIC SYSTEM FOR MANAGED LAUNCH OF NANOSATELLITES
- SPECIAL FEATURES OF LOW-ALTITUDE AERODYNAMICALLY STABILIZED NANOSATELLITE MOVEMENT