Analytical comparison of hydrazine with primary propellants as the turbine drive fluid for hydrogen-fluorine and hydrogen-oxygen altitude stage rockets /
by William T. Wintucky.

Description

Main Author: Wintucky, William T.
Related Names: Lewis Research Center.
Language(s): English
Published: Washington, [D.C.] : National Aeronautics and Space Administration, 1959.
Subjects: Specific impulse.
Mass flow rate.
Turbine pumps.
Rocket engine design.
Propulsive efficiency.
Propulsion system performance.
Propellant tests.
Monopropellants.
Rocket engines.
Liquid propellant.
Engines.
Oxygen.
Hydrogen.
Hydrazines.
High energy propellants.
Note: "NASA TN D-78."
"Lewis Research Center, Cleveland, Ohio."
"October 1959."
Title from cover.
Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 12/05/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890068241_1989068241.pdf.
Physical Description: 26 p. : ill. ; 26 cm.
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