SMALL SPACECRAFT LAUNCHING SYSTEM
Annotation
A classification of small spacecraft according to mass criterion is suggested. Domestic and foreign prototypes and analogs of small spacecraft launching systems are considered, their characteristics are analyzed. Small spacecraft launching system based on research rocket complex MR-30 is proposed. The research rocket complex MR-30 includes newly-developed research meteorological rocket MN-300, the flight level of the rocket being about 300 km. Scientific, technical and economic justifications and offers on modernization of a research rocket complex for its use for problems of small spacecraft launching into low orbits are provided. Requirements to a universal platform of the staff payload of the research rocket in view of minimization of technical means of the onboard equipment of small spacecraft for realization of research and local problems from space locate are substantiated. A plan of modernization of the standard block of MN-300 rocket equipment to use it as a platform for small spacecraft launching at minimal cost is developed. The mass characteristics and dimensions of the rocket and the platform for small spacecraft arrangement are presented. The scheme of rocket experiment for small spacecraft launching to a low orbit by means of the research rocket complex is 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
- PROJECT OF NANOSATELLITE GROUP SEPARATION AT CLUSTER LAUNCHING FROM AN ORBITAL STAGE
- SPECIAL FEATURES OF LOW-ALTITUDE AERODYNAMICALLY STABILIZED NANOSATELLITE MOVEMENT