Books on the topic 'RP-1 rocket propellants'

Masters, Philip A. High-pressure calorimeter chamber tests for liquid oxygen/kerosene (LOX/RP-1) rocket combustion. Cleveland, Ohio: Lewis Research Center, 1988.

Kearns, Kimberly A. The revamping of an ignition test facility. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2002.

Magee, Joseph W. Thermophysical properties measurements and models for rocket propellant RP-1: Phase I. Boulder, Colo: U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 2007.

S, Zakany James, and United States. National Aeronautics and Space Administration., eds. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket combustion experiments. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

S, Zakany James, and United States. National Aeronautics and Space Administration., eds. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket combustion experiments. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

S, Zakany James, and United States. National Aeronautics and Space Administration., eds. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket heat transfer and combustion measurements. [Washington, D.C: National Aeronautics and Space Administration, 1996.

S, Zakany James, and United States. National Aeronautics and Space Administration., eds. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket heat transfer and combustion measurements. [Washington, D.C: National Aeronautics and Space Administration, 1996.

United States. National Aeronautics and Space Administration., ed. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket engine calorimeter heat transfer measurements and analysis. [Washington, D.C.]: National Aeronautics and Space Administration, 1997.

United States. National Aeronautics and Space Administration., ed. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket engine calorimeter heat transfer measurements and analysis. [Washington, D.C.]: National Aeronautics and Space Administration, 1997.

S, Armstrong Elizabeth, Price Harold G, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. High-pressure calorimeter chamber tests for liquid oxygen/kerosene (LOX/RP-1) rocket combustion. [Washington, DC]: National Aeronautics and Spac14., 1988.

S, Armstrong Elizabeth, Price Harold G, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. High-pressure calorimeter chamber tests for liquid oxygen/kerosene (LOX/RP-1) rocket combustion. [Washington, DC]: National Aeronautics and Spac14., 1988.

Center, Lewis Research, ed. Modification of the SHABERTH bearing code to incorporate RP-1 and a discussion of the traction model. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

Center, NASA Glenn Research, ed. The revamping of an ignition test facility. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2002.

Characterization of aluminum/RP-1 gel propellant properties. [Washington, DC]: National Aeronautics and Space Administration, 1988.

Characterization of aluminum/RP-1 gel propellant properties. [Washington, DC]: National Aeronautics and Space Administration, 1988.