GAS-PHASE NUCLEAR ROCKET ENGINE WITH THRUST AUGMENTATION Russian patent published in 1995 - IPC

Abstract RU 2041392 C1

FIELD: space engineering. SUBSTANCE: to augment thrust air is injected in nozzle 2. The air is supplied through air intake 3, which is in communication with the space of nozzle 2, and passageway 8 for additional supplying of air stored up on the board. Turbofan blowers 4 are used for air injection at low flying speed. EFFECT: enhanced efficiency. 2 cl, 2 dwg

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RU 2 041 392 C1

Authors

Vojtko V.V.

Potupalo N.V.

Vojtko I.V.

Dates

1995-08-09Published

1991-07-03Filed