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The Use of Auxiliary Rockets in High‐Speed Aircraft: An Analysis of the Possibilities of Rockets as Thrust Augmenters

Dipl. Ing. Zb. Plaskowski (Institut fur Aerodynamik, E.T.H., Zurich.)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 March 1951

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Abstract

ALTHOUGH a new epoch in high‐speed flight opened with the introduction of the jet propulsion engine, new problems were presented by the thrust characteristics and high fuel‐consumption of the gas turbine.

Citation

Plaskowski, Z. (1951), "The Use of Auxiliary Rockets in High‐Speed Aircraft: An Analysis of the Possibilities of Rockets as Thrust Augmenters", Aircraft Engineering and Aerospace Technology, Vol. 23 No. 3, pp. 72-75. https://doi.org/10.1108/eb032008

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MCB UP Ltd

Copyright © 1951, MCB UP Limited