SPACE-MISSION ROCKET Russian patent published in 2009 - IPC B64G1/00 

FIELD: transportation.

SUBSTANCE: space-mission rocket comprises packet of rocket blocks. Blocks comprise instruments of control systems, tanks of fuel components, cruise and vernier liquid propellant rocket engines. Cylindrical part of head fairing body is arranged with ratio of its diametre to diametre of the third stage block body within the limits from 1.39 to 1.6 and ratio of height to its diametre within the limits from 1.2 to 1.65 and is connected by transition compartment of conical shape with the third stage block. Height of transition compartment and cylindrical shell of the third stage block fuel tank is arranged as not more than 1.6 of difference between diametres of head fairing and fuel tank body arranged in the form of bearing cylindrical part of the third stage block structure with lower spherical bottom of diametre more than diametre of the third stage block body. Sealing gaskets are fixed on joined surfaces of head fairing and transition compartment folds. Drain valves for excessive internal pressure are fixed on cylindrical part of dropped folds of head fairing body. On longitudinal-transverse power set and bearing shell of intertank compartment body of the third stage block, two stringers are fixed, which are rigidly connected between each other by cantilever platform to fix unit of angular speed detector in control system.

EFFECT: increased dimensions of payload transported by space-based rocket.

13 dwg