Hostname: page-component-7479d7b7d-wxhwt Total loading time: 0 Render date: 2024-07-12T04:22:24.787Z Has data issue: false hasContentIssue false

Liquid Propellant Rocket Motors

Published online by Cambridge University Press:  28 July 2016

B. R. Diplock
Affiliation:
The de Havilland Engine Co. Ltd.
D. L. Lofts
Affiliation:
The de Havilland Engine Co. Ltd.
R. A. Grimston
Affiliation:
The de Havilland Engine Co. Ltd.

Extract

It has been said that a rocket motor is the simplest “ prime mover.” This is correct in theory, since fundamentally a rocket consists of a chamber containing a gas under pressure, having a nozzle at one end through which the gas expands, forming a propulsive jet. Since the pressure ratio of the rocket is always greater than the critical pressure ratio, the nozzle is invariably of the convergent-divergent or de Laval type in which the velocity is subsonic up to the throat, sonic at the throat and supersonic in the divergent portion.

It is a popular fallacy that a rocket or jet engine obtains a forward thrust by allowing the rearward jet of gas to push against the atmosphere in which it is operating. This is not correct and it can be proved that a rocket will operate successfully, and more efficiently, in a vacuum.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1953

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

Three papers read before the Graduates' and Students' Section of the Society on 4th November 1952.