| 摘要 |
FIELD: aircraft engineering.SUBSTANCE: flying launcher comprises cluster of tanks, fasteners, wing, engine and payload. Said cluster of tanks comprises two pairs of identical-volume cylindrical tanks with rocket liquid propellant of equal density and equal volume flow. Said four tanks are secured to each other by reinforcing belts to make parts of tanks with invariable center of gravity at efflux of propellant. Fasteners are secured to two tanks to allow attachment of the wing thereto. Linkage of tanks is arranged at top stage of square section and rounded angles.EFFECT: decreased length of launcher.4 cl, 5 dwg |
