| 摘要 |
FIELD: space industry. ^ SUBSTANCE: proposed fuselage contains skin, framework load-bearing members and axially-symmetric magnetic elements to control high-temperature flow around fuselage arranged inside and along fuselage with contours similar to contours of skin in cross section of fuselage. Magnetic elements are made in form of load-bearing members of framework. ^ EFFECT: reduced weight. ^ 3 dwg |
