초록 ▼

The invention relates to a space-rocket technology an can be used for both a pilot-controlled and unpiloted space craft in the earth's orbit. The inventive method consists in igniting-up cruising liquid-fuel rocket engines (LRE) of all assembly units, when the propulsion power of LRE of the side uni

The invention relates to a space-rocket technology an can be used for both a pilot-controlled and unpiloted space craft in the earth's orbit. The inventive method consists in igniting-up cruising liquid-fuel rocket engines (LRE) of all assembly units, when the propulsion power of LRE of the side units is set to maximum and the LRE of the central unit is set relatively low.

대표청구항 ▼

1. A multifunctional launch vehicle of a combined scheme with cruise LRESs, the launch vehicle comprising a lower multiunit assembly of rocket units with cruise LRESs, including a central and connected thereto side rocket units and tandem secured on the central unit a transition compartment, acceler

1. A multifunctional launch vehicle of a combined scheme with cruise LRESs, the launch vehicle comprising a lower multiunit assembly of rocket units with cruise LRESs, including a central and connected thereto side rocket units and tandem secured on the central unit a transition compartment, acceleration rocket units and a head unit with a payload, head domes of side rocket units, and a system for securing the side rocket units to the central unit, characterized in that the lower multiunit assembly is composed of identical rocket units having identical propellant tanks and identical cruise LRESs with adjustable thrust, secured in a gimbal suspension, the side rocket units are mounted on the central rocket unit symmetrically relative to its longitudinal axis in sectors formed by swinging planes of the cruise LRES of the central rocket unit so that the swinging planes of the cruise LRES of each side rocket unit are parallel to corresponding swinging planes of the cruise LRES of the central rocket unit. 2. A multifunctional launch vehicle of a combined scheme with cruise LRESs, the launch vehicle comprising a lower multiunit assembly of rocket units with cruise LRESs, including a central and connected thereto two side rocket units mounted on the central rocket unit in a single plane symmetrically relative to the longitudinal axis of the central rocket unit, and tandem secured on the central unit a transition compartment, acceleration rocket units and a head unit with a payload, head domes of side rocket units, and a system for securing the side rocket units to the central unit, characterized in that the lower multiunit assembly is composed of identical rocket units having identical propellant tanks and identical cruise LRESs at a thrust adjustable within the range of from 30% to 100%, secured in a gimbal suspension, the side rocket units are mounted on the central rocket unit in sectors formed by swinging planes of the cruise LRES of the central rocket unit in a plane that is oriented at an angle of 45° to one of the swinging planes of the cruise LRES of the central rocket unit, so that the swinging planes of the cruise LRES of each side rocket unit are parallel to corresponding swinging planes of the cruise LRES of the central rocket unit. 3. A multifunctional launch vehicle of a combined scheme with cruise LRESs, the launch vehicle comprising a lower multiunit assembly of rocket units with cruise LRESs, including a central and connected thereto four side rocket units mounted on the central rocket unit in two mutually perpendicular planes symmetrically relative to the longitudinal axis of the central rocket unit, and tandem secured on the central unit a transition compartment, acceleration rocket units and a head unit with a payload, head domes of side rocket units, and a system for securing the side rocket units to the central unit, characterized in that the lower multiunit assembly is composed of identical rocket units having identical propellant tanks and identical cruise LRESs at a thrust adjustable within the range from 30% to 100%, secured in a gimbal suspension, the side rocket units are mounted on the central rocket unit in sectors formed by swinging planes of the cruise LRES of the central rocket unit in planes that are oriented at an angle of 45° to the swinging planes of the cruise LRES of the central rocket unit, so that the swinging planes of the cruise LRES of each side rocket unit are parallel to corresponding swinging planes of the cruise LRES of the central rocket unit.