FIELD: weapons and ammunition.
SUBSTANCE: rolling missile is accelerated to cruising speed by means of a detachable solid-fuel launching accelerator, cruising speed is maintained with thrust of a small-size disposable turbo-jet engine, twisted and a mode of rotation about the roll axis is maintained by means of aft stabilisers that are slanted relative to the longitudinal axis and/or a gas-dynamic nozzle on the turbo-jet engine, aerodynamic lifting force is formed in the rotation mode by means of n pairs of small-size foldable wings.
EFFECT: invention allows increasing flight distance of a cruise missile.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ROLLING CRUISE MISSILE | 2014 |
|
RU2544446C1 |
| AIRCRAFT | 2007 |
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