FIELD: weapons and ammunition.
SUBSTANCE: single-stage booster comprises one or more liquid rocket engines, a fuel tank with tanks of fuel and oxidiser, one or more pairs of hinged fuel tanks of fuel and oxidiser, respectively connected with the tanks of fuel and oxidiser of the fuel tank. The hinged fuel tanks diametrically located with respect to each other are connected to the fuel tank of the propulsion system with the ability of separation after fuel depletion.
EFFECT: invention enables to carry out the launching from any terrain, excludes the area of falling the waste parts of the booster.
6 dwg
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Authors
Dates
2014-06-10—Published
2012-10-24—Filed