FIELD: aircraft engineering.
SUBSTANCE: invention relates to aerospace engineering and can be used in spacecraft landing gear. Proposed device comprises leg composed of barrel with inner damper connected with plain pivot and, telescopically, with moving rod, ball joint, support plate, two ropes secured without slack and made of super modulus material to limit angular displacement of said support and to reset it to initial position and mechanism of unilateral turn of said support. Angle between leg lengthwise axis at the pate working position and the straight line extending through spherical joint centre is parallel with spacecraft lengthwise axis depends upon angle of friction and spacecraft approach angle relative to lading site.
EFFECT: reduced impact loads.
1 dwg
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