FIELD: physics.
SUBSTANCE: invention relates to the field of information, in particular to methods for generating visually perceptible information. Method of generating visually perceptible information involves formation of an image from orbits of artificial satellites of the planet, wherein the artificial satellites are brought into orbit in advance as part of the carrier space vehicle, when creating an orbital image, artificial satellites are separated from a carrier device and impart a pulse of characteristic speed of up to 500 m/s so that, moving along their own trajectories, they enter a visual observation zone at altitude of 60...100 km in certain program moment of orbital image formation, at that pyrophoric materials are introduced into composition of artificial satellites.
EFFECT: technical result consists in realizing visually observed short-lived images such as salute (fireworks, meteoric rain), covering a significant part of the firmament above the observation zone.
5 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD FOR GROUP ORBITAL FLIGHT OF ARTIFICIAL SATELLITES | 2011 |
|
RU2592121C2 |
METHOD FOR BROADCASTING OF VISUAL INFORMATION | 1991 |
|
RU2093967C1 |
METHOD OF INCREASE OF TERMS OF SPACECRAFT ACTIVE-FLIGHT TIME | 1996 |
|
RU2166464C2 |
METHOD OF GROUP ORBITAL FLIGHT OF ARTIFICIAL SATELLITES | 2014 |
|
RU2569236C1 |
METHOD OF INCREASE OF ACTIVE EXISTENCE OF SPACE VEHICLES | 1995 |
|
RU2136551C1 |
METHOD OF DETERMINATION OF SPACE STATION MASS IN FLIGHT | 2005 |
|
RU2301181C2 |
ARTIFICIAL EARTH SATELLITE | 2014 |
|
RU2579600C1 |
METHOD FOR EXTENDING ACTIVE PERIOD OF SPACE VEHICLES | 1996 |
|
RU2137682C1 |
METHOD AND SYSTEM FOR INJECTION OF SPACECRAFT INTO DESIRED ORBIT BY MEANS OF ENGINES POSSESSING HIGH SPECIFIC IMPULSE | 1997 |
|
RU2212363C2 |
METHOD OF LIMITATION OF POLLUTING OF OPERATING AREAS OF GEOSPACE | 2017 |
|
RU2665156C1 |
Authors
Dates
2019-10-31—Published
2018-01-11—Filed