FIELD: transport.
SUBSTANCE: invention relates to aerospace engineering, particularly, to space rocket head design. Space rocket head consists of nose cone and spacecraft. Space rocket head comprises intermediate compartment connecting spacecraft with carrier rocket and nose cone by means of throw-off connections. Spacecraft propulsion module is located inside intermediate compartment, outside dislodgement zone of intermediate compartment separated from spacecraft together with rocket carrier. Intermediate compartment top frame has two end plug-in joints to be separated in flight and connecting said compartment to nose cone and spacecraft.
EFFECT: decreased weight of rocket, increased useful space under nose cone.
4 dwg
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