SU1839928A1 - Electromechanical actuating member for spacecraft orientation and stabilization system - Google Patents
Electromechanical actuating member for spacecraft orientation and stabilization systemInfo
- Publication number
- SU1839928A1 SU1839928A1 SU2274223/11A SU2274223A SU1839928A1 SU 1839928 A1 SU1839928 A1 SU 1839928A1 SU 2274223/11 A SU2274223/11 A SU 2274223/11A SU 2274223 A SU2274223 A SU 2274223A SU 1839928 A1 SU1839928 A1 SU 1839928A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- actuating member
- flywheel
- electromechanical actuating
- stabilization system
- motor
- Prior art date
Links
Abstract
FIELD: spacecraft equipment.SUBSTANCE: proposed electromechanical actuating member has body, electric motor with flywheel, tachogenerator and control unit for control of precision motion of motor-flywheel connected with two torque sensors. Body is spherical and form and is provided with three intersecting circular grooves. Motor-flywheel is mounted in body by means of trunnions. Retainers electrically connected with control unit are mounted in point of intersection of body grooves.EFFECT: reduced mass and overall dimensions.5 dwg
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU2274223/11A SU1839928A1 (en) | 1980-03-07 | 1980-03-07 | Electromechanical actuating member for spacecraft orientation and stabilization system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU2274223/11A SU1839928A1 (en) | 1980-03-07 | 1980-03-07 | Electromechanical actuating member for spacecraft orientation and stabilization system |
Publications (1)
Publication Number | Publication Date |
---|---|
SU1839928A1 true SU1839928A1 (en) | 2006-06-20 |
Family
ID=60541553
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU2274223/11A SU1839928A1 (en) | 1980-03-07 | 1980-03-07 | Electromechanical actuating member for spacecraft orientation and stabilization system |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU1839928A1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2555080C2 (en) * | 2008-10-31 | 2015-07-10 | Таль | Method and system to rule out saturation of spacecraft inertial wheels |
EA028853B1 (en) * | 2015-07-07 | 2018-01-31 | федеральное государственное автономное образовательное учреждение высшего образования "Самарский государственный аэрокосмический университет имени академика С.П. Королева (национальный исследовательский университет)" (СГАУ) | Method of spatial reorientation and change of parameters of spacecraft angular motion |
-
1980
- 1980-03-07 SU SU2274223/11A patent/SU1839928A1/en active
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2555080C2 (en) * | 2008-10-31 | 2015-07-10 | Таль | Method and system to rule out saturation of spacecraft inertial wheels |
EA028853B1 (en) * | 2015-07-07 | 2018-01-31 | федеральное государственное автономное образовательное учреждение высшего образования "Самарский государственный аэрокосмический университет имени академика С.П. Королева (национальный исследовательский университет)" (СГАУ) | Method of spatial reorientation and change of parameters of spacecraft angular motion |
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