A study of several parameters controlling the trajectories of a supersonic antiaircraft missile powered with solid- or liquid-fuel rockets Page: 1 of 43
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:
A STUDY OF SEVERAL PARAMETERS CONTROLLING THE
TRAJECTORIES OF A SUPERSONIC ANTIAIRCRAFT MISSILE
POWERED WITH SO LID- OR LIQUID-FUEL ROCKETS
By Ralph F. Huntsberger
Ames Aeronautical Laboratory
Moffett Field, Calif.
Stt contains classified information affeo-
fense of the United States within
tne onage LO, uS C .:31 n .uuL.
Its transom tion of its contents in
any manner to an is prohibited by
law. Information so al imparted only
to persons in the military an a of the
United States, appropriate civilian em-
ployees of the Federal Government who -
Imate interest therein, and to United States
of known loyalty and discretion who of necessity
be informed thereof.
NATIONAL ADVISORY COM t
-April 24, 1947
RM No. A6G22
ACA MR li
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.
Huntsberger, Ralph F. A study of several parameters controlling the trajectories of a supersonic antiaircraft missile powered with solid- or liquid-fuel rockets, report, April 24, 1947; (digital.library.unt.edu/ark:/67531/metadc57965/m1/1/: accessed October 23, 2017), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.