![Scientific and technical journal «Priborostroenie»](/images/mag-pr.png)
PERSPECTIVES OF SMALL SIZE SPACECRAFT DEVELOPMENT FOR VARIOUS PURPOSES AT JSC RUSSIAN SPACE SYSTEMS
![Scientific and technical journal «Priborostroenie»](/images/mag-pr.png)
Annotation
In 2015, 10 years since the launch of the first technological nanosatellite TNS-0 N1 developed by JSC Russian Space Systems (JSC RSS) was marked. Despite the relatively simple structure and small size of TNS-0 N1 (total weight was less than 5 kg), it was successfully used as a platform for testing a number of new technologies and systems modern at that time: new principles to be applied for the purpose of rocket and space equipment development, single-point control of a satellite via space system GLOBALSTAR, new samples of Sun and horizon sensors, as well as certification of COSPAS-SARSAT beacons, etc. The paper presents JSC RSS experience in nanosatellites development, as well as concepts of a number of technologies and nanosatellite systems suitable for pilot projects implementation. Several problems of development of perspective technologies of space instrument manufacturing are discussed, the possibility of carrying out scientific research and technological works compensating the difference in levels of technological readiness of elements of the service subsystems and the target hardware is considered. It is proposed to perform an analysis of domestic technology service and on-bard radio systems for small spacecraft with the objective of achieving a qualitatively new level of implementation of design works. The necessity to restore the concept of scientific-technological research works and their inclusion in the Federal Space Program, and in other Federal target programs is declared. Results of the works on creation of various useful loadings intended for placement on the nanosatellites of CubeSat format are presented.
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Articles in current issue
- 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
- PROJECT OF NANOSATELLITE GROUP SEPARATION AT CLUSTER LAUNCHING FROM AN ORBITAL STAGE
- SPECIAL FEATURES OF LOW-ALTITUDE AERODYNAMICALLY STABILIZED NANOSATELLITE MOVEMENT