Relation of turbojet propulsion system development to the strategic bomber mission Page: 2 of 32
This report is part of the collection entitled: National Advisory Committee for Aeronautics Collection and was provided to Digital Library by the UNT Libraries Government Documents Department.
The following text was automatically extracted from the image on this page using optical character recognition software:
NACA RM S56H07
NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS
Air Research and Development Command, U. S. Air Force
RELATION OF TURBOJET PROPULSION SYSTEM DEVELOPMENT
TO THE STRATEGIC BOMBER MISSION*
By Addison M. Rothrock, Richard S. Cesaro, and Curtis L. Walker
A generalized analysis presents the effects of turbojet propulsion
system development and fuel selection on ability of a strategic bomber
to perform desired and minimum missions. The variation of bomber per-
formance using a hydrocarbon, boron, or nuclear fuel is discussed. With
chemical fuel, the effects of refueling are discussed. With nuclear fuel,
the nuclear cruise-chemical dash bomber and the nuclear subsonic tug tow-
ing a chemically powered supersonic bomber are compared. The factors
that determine bomber gross weight and bomber altitude are briefly
In planning the defenses of the country, it is desirable to examine
continually the technical likelihood of meeting operational requirements
set by the strategic bomber mission. A technical evaluation should pre-
sent the different methods by which these operational requirements can
be met, or, if they cannot be met, offer a comparison of the alternatives
that are currently technically possible. This report makes such an eval-
uation, and presents it in terms intended to be understandable to per-
sonnel not intimately familiar with the procedures of such analyses.
An examination is made of the interrelations between the basic var-
iables that determine bomber range, gross weight, and flight altitude.
Estimates are made of probable improvements that can be made in the pro-
pulsion factors, and of the resulting improvements in bomber range. To
a certain extent, the current discussion is a continuation of that pre-
sented in reference 1.
This analysis was made at the request of the U. S. Air Force and
has been presented orally to various USAF groups.
Here’s what’s next.
This report can be searched. Note: Results may vary based on the legibility of text within the document.
Tools / Downloads
Get a copy of this page or view the extracted text.
Citing and Sharing
Basic information for referencing this web page. We also provide extended guidance on usage rights, references, copying or embedding.
Reference the current page of this Report.
Rothrock, A. M.; Cesaro, R. S. & Walker, C. L. Relation of turbojet propulsion system development to the strategic bomber mission, report, August 15, 1956; (digital.library.unt.edu/ark:/67531/metadc53305/m1/2/: accessed November 18, 2017), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.