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Flight Test of the Aerojet 7KS-6000 T-27 Jato Rocket Motor
"A flight test of the Aero jet Engineering Corporation's 7KS-6000 T-27 Jato rocket motor was conducted at the Langley Pilotless Aircraft Research Station at Wallops Island, Va, to determine the flight performance characteristics of the motor. The flight test imposed an absolute longitudinal acceleration of 9.8 g upon the rocket motor at 2.8 seconds after launching. The total impulse developed by the motor was 43,400 pound-seconds, and the thrusting time was 7.58 seconds" (p. 1).
Date:
December 20, 1949
Creator:
Bond, Aleck C. & Thibodaux, Joseph G., Jr.
System:
The UNT Digital Library
A Free-Flight Technique for Measuring Damping in Roll by Use of Rocket-Powered Models and Some Initial Results for Rectangular Wings
Report presenting a simplified method for obtaining free-flight measurements of damping in roll through the use of rocket-powered models. Initial configurations have been tested for a range of Mach numbers. Results regarding the rolling velocity with two different airfoil sections and damping-in-roll coefficient are provided.
Date:
December 20, 1949
Creator:
Edmondson, James L. & Sanders, E. Claude, Jr.
System:
The UNT Digital Library
The Densities of Tributyl Phosphate - Carbon Tetrachloride Solutions Containing Uranium and Nitric Acid
The following report provides the analysis of a large number of unreported data--taken during a study described in report HW-15230--containing density values obtained for solutions of uranium and nitric acid in tributyl phosphate-carbon tetrachloride solutions.
Date:
December 20, 1949
Creator:
Moore, Robert Lee
System:
The UNT Digital Library
Level and Leak Indicators
The following report provides results taken from a sodium level indicator developed at Sacandaga using electrical resistance as the principle.
Date:
December 20, 1949
Creator:
Vandenberg, L. B.
System:
The UNT Digital Library