A study of several parameters controlling the trajectories of a supersonic antiaircraft missile powered with solid- or liquid-fuel rockets Page: 1 of 43
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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
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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 September 18, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.