An inter-stage rocket booster, converts kinetic energy spent stages in additional impetus THRUST (OPTIONS)

摘要

This solution is designed for the multi-stage launch vehicles for various purposes with different types of power plants. Scope covers missiles as science and technology, and military applications, with any type of jet propulsion. The technical result of the utility model is the relative simplicity of design, increased reliability, reduction of the impact load in the separation steps, the complete absence of the fragments, the rapid removal stage detachable to a safe distance, and to create an additional high-power pulse of thrust (acceleration). This leads to fuel savings, reduction in design weight, reduce missile costs and a considerable increase in the efficiency of its propulsion system. Furthermore, the described apparatus can be taken both in new and in existing launch vehicles through their minor modifications (retrofitting). At the same time to modernize the missile does not require any substantial design changes - the device is placed in the existing Interstage technological openings. The use of this device allows you to quickly increase capacity and efficiency of virtually all existing launch vehicles, which is of strategic importance, for example, to improve the country's military capabilities. The use of utility model can not only quickly improve the efficiency (effectiveness) of existing space-rocket systems, but also to create a fundamentally new-a new generation of missile with a more compact and much more efficient power plant. Said scientific and technical result is achieved due to the fact that the inter-stage rocket booster comprising piropatorny with EB, characterized in that it consists of several trunks, each of which has a cutter with EB, wherein each barrel laid plunger rod with shock absorber for mitigating force when the cutter repellent detachable part (step) missile in a direction opposite the direction of the missile.