FIELD: rocketry; all-azimuth injection complexes without alienation of land for fields of fall of rocket pods. SUBSTANCE: booster has air-breathing jet engines with fairings and service and balancing tanks. All moving wing (through angle of 90 deg) with propellant tanks inside it is mounted at top of case. Fin and stabilizer are mounted on tail section; they have form of swivel panels at small V-shaped negative angle. Booster is also provided with three-leg landing gear, fore spherical fairing and units for mating with second stage of launch vehicle. EFFECT: possibility of creation of unified carrier both of cluster and tandem configuration; improved balancing and other characteristics in return flight of used booster of first stage. 7 cl, 11 dwg
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