About this scholarly article

12th Propulsion Conference - A review of the Mark 48-F, 3.50 pitch diameter, 2-stage reaction turbine designed for the staged combustion cycle requirements of an advanced space engine by MACALUSO, S. is a scholarly article available to read on EtoBox.

Author

MACALUSO, S.

Publisher

American Institute of Aeronautics and Astronautics

Published

1976

Language

EN