FIELD: test.
SUBSTANCE: invention relates to test equipment and can be used for simulation of zero-gravity at ground development of transformable systems (TS) of spacecrafts. Method includes connection of TS (1, 2) installed on support (3), cable (4) through the system of units (5) with counterbalance (6, 7) connected to support post (8). Counterweight is made in the form of a mechanism with an identical TS kinematic circuit and is arranged symmetrically to the TS relative to some horizontal plane. If observing identical transformation sequence of TS and counterweight, required compensation of forces of gravity of links of TS is achieved.
EFFECT: technical result is simplification of provision of variable TS weight-bearing force during its development.
1 cl, 1 dwg
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