FIELD: space engineering; stabilizing units for well-defined orientation of spacecraft. SUBSTANCE: transportation unit and functional units ensuring operation of gravitational device rod are used after injection of spacecraft as gravitational weight. EFFECT: increased utilization factor of spacecraft mass; reduced mass of spacecraft. 3 cl, 2 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF PRODUCING SPACESHIP THERMAL CONTROL SYSTEM AND DEVICE TO THIS END | 2009 |
|
RU2436716C2 |
TURNTABLE FOR SECURING PAYLOAD | 2003 |
|
RU2238888C1 |
DEVICE FOR FORMING WEIGHTLESSNESS OF LOW-RIGIDITY MECHANICAL SYSTEM OF SPACECRAFT MOVING VERTICALLY | 2004 |
|
RU2273592C2 |
MICRO-SATELLITE | 2004 |
|
RU2268205C2 |
METHOD AND DEVICE FOR SINGLE-AXIS GRAVITATIONAL ATTITUDE CONTROL OF AXISYMMETRICAL SPACECRAFT IN ORBIT OF EARTH SATELLITE | 1996 |
|
RU2128608C1 |
EXTENDABLE BOOM DEVICE | 2021 |
|
RU2772764C1 |
DEVICE FOR SPACECRAFT GRAVITATIONAL STABILIZATION | 2005 |
|
RU2304069C2 |
SPACECRAFT FOR DELIVERING PAYLOAD TO SPACE BODY WITH SMALL GRAVITATIONAL FIELD | 2020 |
|
RU2758656C1 |
ACTIVE DEVICE FOR FIXATION OF PAYLOAD, PRIMARILY TO BODY OF ORBITAL SPACECRAFT | 2014 |
|
RU2583993C2 |
METHOD FOR FORMING PAYLOAD SEPARATION SYSTEM | 2004 |
|
RU2293691C2 |
Authors
Dates
2004-02-20—Published
2001-04-09—Filed