PROSPECTS OF REALIZATION OF PROTO-FLIGHT APPROACH IN NANOSATELLITE GROUND TESTING
Annotation
Perspective schematic of realization of proto-flight approach in ground testing of nanosatellites is presented. The approach presupposes performing qualification flight tests with the single manufactured sample. Advantages and disadvantages of the proposed approach are discussed. To reduce the impact of identified disadvantages, it is proposed to use computational models of reliability available in a range of organizations of the rocket and space industry. Extension of the software base is supposed to be advisable in the frames of the of the future program "Creation of scientific-educational space system of the Union state", including the establishment of specialized ground-based functional modules to predict residual life and reliability of onboard systems of nanosatellites on the base of comprehensive tests results.
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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
- 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