Title:
ROCKET ENGINE WITH TURBO-FAN
Document Type and Number:
Japanese Patent JPS5215918
Kind Code:
A
Abstract:
PURPOSE: A rocket engine equipped with turbo-fan, that realizes to provide transport of pay load with less propulsion agent when a plane makes ascendance in low height, low height altitude by rocket engine jet power and turbo-fan propulsion power in rotating turbo-fan with gas etc. produced at the rocket engine combustion chamber.
Inventors:
KUSANO MASAAKI
Application Number:
JP9241675A
Publication Date:
February 05, 1977
Filing Date:
July 28, 1975
Export Citation:
Assignee:
KUSANO MASAAKI
International Classes:
F02K9/00; F02K5/00; (IPC1-7): F02K5/00; F02K9/00