FIELD: transport.
SUBSTANCE: invention relates aerospace engineering, namely, to design of spacehead. The spacehead consists of head fairing, missile upper stage with instrumental framework, adapter representing tapered cone and spacecraft. The intersection line of the plane passing through longitudinal axis of spacehead and the plane formed by two axes of adjacent rods of upper stage instrumental framework where the point of intersection of these axes is located at the place of adapter connection to the mentioned framework is the extension of adapter generatrix.
EFFECT: better mass parameters of spacehead and increase of payload zone in underfairing area of spacehead.
1 dwg
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Authors
Dates
2011-06-27—Published
2009-12-21—Filed