FIELD: test equipment.
SUBSTANCE: invention relates to test equipment, and more specifically to tests of precision opened structures of spacecraft. Device for weightlessness of precision opened structures of spacecraft comprises two-arm lever, on one end of which there fixed is object to be weightlessed, and on the other balancing weight. Double-arm lever is equipped with hinged device with horizontal and vertical axes of rotation. There is a sensor for determining unloading force and a metal band with tension units. Adjustment of balanced state of two-arm lever relative to point of intersection of horizontal and vertical axes of hinge device is provided with yokes with threaded pins, balancing weights. Presence of elements of optical control – reference signs, provides accurate determination of position in space of point of intersection of horizontal and vertical axes of hinged device of double-arm lever and point, which is center of plug for attachment of suspension.
EFFECT: higher accuracy.
1 cl, 6 dwg
Title | Year | Author | Number |
---|---|---|---|
ROTARY DEVICE WITH A BLOCK AND TACKLE SYSTEM FOR WEIGHLESSING OPEN STRUCTURES OF A SPACECRAFT | 2019 |
|
RU2721448C1 |
SYSTEM OF SIMULATING WEIGHTLESSNESS | 2014 |
|
RU2565807C2 |
WEIGHT-LOSS SYSTEM | 2018 |
|
RU2697632C1 |
CROSSARM | 2017 |
|
RU2703861C2 |
DEVICE OF MECHANISM WEIGHTLESSNESS SIMULATION WITH FLEXIBLE STRUCTURE OF ELEMENTS | 2006 |
|
RU2334970C2 |
SOLAR BATTERY OPENING TEST BENCH | 2010 |
|
RU2468969C2 |
PLANT FOR TESTING SIZABLE SOLAR CELL BATTERIES | 0 |
|
SU1803351A1 |
BENCH FOR OPENING PANELS OF SOLAR BATTERY | 2011 |
|
RU2483991C1 |
PROCEDURE MEASURING THRUST FORCE OF JET ENGINE AND BED FOR ITS REALIZATION | 2001 |
|
RU2221995C2 |
DEVICE FOR FORMING WEIGHTLESSNESS OF LOW-RIGIDITY MECHANICAL SYSTEM OF SPACECRAFT MOVING VERTICALLY | 2004 |
|
RU2273592C2 |
Authors
Dates
2020-09-28—Published
2019-08-14—Filed