FIELD: astronautics.
SUBSTANCE: invention relates to spacecraft docking means during their withdrawal and subsequent detachment in space. Dispenser (adapter) (1), mainly small spacecrafts (microsatellites), consists of circular structure with several ports (2) for spacecraft installation. Surface (3) of annular structure is made partially or completely spherical.
EFFECT: technical result consists in more convenient fixation of small satellites and reduced weight of adapter structure.
5 cl, 3 dwg
Title | Year | Author | Number |
---|---|---|---|
INCLINED ADAPTER FOR TRANSPORTATION OF SEVERAL PAYLOADS ON ONE LAUNCH VEHICLE | 1996 |
|
RU2155146C2 |
SPACECRAFT SERVICING DEVICES AND CORRESPONDING NODES, SYSTEMS AND METHODS | 2018 |
|
RU2765040C2 |
SPACECRAFT SERVICING DEVICES AND CORRESPONDING NODES, SYSTEMS AND METHODS | 2018 |
|
RU2765065C2 |
CONCEPT OF AN EFFICIENT SATELLITE STRUCTURE FOR SINGLE OR STACKED GROUP LAUNCHES | 2019 |
|
RU2773764C1 |
SPACECRAFT SERVICING DEVICES AND CORRESPONDING NODES, SYSTEMS AND METHODS | 2018 |
|
RU2765021C2 |
ADAPTER FOR WAY LOOSE OF USEFUL LOAD | 2016 |
|
RU2624959C1 |
SPACE HEAD FOR GROUP LAUNCH OF SATELLITES | 2010 |
|
RU2428358C1 |
SPACESHIP HEAD | 2014 |
|
RU2569966C1 |
SPACE HEAD MODULE FOR ISOLATED AND CLUSTER LAUNCH OF SATELLITES | 2005 |
|
RU2293689C2 |
UNIVERSAL SPACE TRANSPORT SYSTEM BASED ON FAMILY OF SPACE ROCKETS OF LIGHT, MEDIUM AND HEAVY CLASSES WITH CARRIER ROCKETS LAUNCHING OVER WATER AREA OF WORLD OCEAN | 2018 |
|
RU2729912C1 |
Authors
Dates
2020-02-03—Published
2015-12-18—Filed