FIELD: aircraft engineering.
SUBSTANCE: claimed invention can be used for destruction of space refuse fragments. Gel-like explosive is secured at the space refuse fragment surface. The blast is initiated by the controlled fuse. The space interceptor is launched to the space refuse fragment.
EFFECT: higher efficiency of large fragment destruction.
1 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF CHANGE OF FLIGHT TRAJECTORY OF OBJECT IN FORM OF LARGE METEORITE, ASTEROID OR COMET NUCLEUS, WITH ITS DEVIATION ASIDE FROM EARTH ORBIT | 2014 |
|
RU2547315C1 |
METHOD OF DESTRUCTING SPACE DEBRIS FRAGMENTS | 2011 |
|
RU2462401C1 |
METHOD OF DESTRUCTION OF PARTS OF WASTE SPACECRAFTS AND DEVICE FOR ITS IMPLEMENTATION | 2016 |
|
RU2637007C1 |
DEVICE FOR DESTRUCTION OF POTENTIALLY DANGEROUS SPACE OBJECTS | 2018 |
|
RU2688111C1 |
METHOD OF DESTRUCTING SPACE REFUSE | 2011 |
|
RU2474516C1 |
DEVICE FOR EARTH PROTECTION FROM SPACE OBJECTS | 2015 |
|
RU2607384C2 |
METHOD OF BREAKING FRAGMENTS OF SPACE DEBRIS | 2002 |
|
RU2204508C1 |
DEVICE FOR CLEANING NEAR EARTH SPACE FROM LARGE-SIZE SPACE DEBRIS | 2019 |
|
RU2721368C1 |
ASTEROID, COMET NUCLEUS AND OTHER SPACE OBJECTS PATH CHANGING DEVICE | 2015 |
|
RU2608193C1 |
SPACE OBJECTS PATH CHANGING DEVICE | 2015 |
|
RU2604902C2 |
Authors
Dates
2016-01-10—Published
2014-08-28—Filed