Books on the topic 'Electric Propellant'

Zurawski, Robert L. Catalytic ignition of hydrogen and oxygen propellants. [Washington, DC: National Aeronautics and Space Administration, 1988.

Whalen, Margaret V. Compatibility of grain-stabilized platinum with candidate propellants for resistojets. [Washington, DC]: National Aeronautics and Space Administration, 1985.

Whalen, Margaret V. Compatibility of grain-stabilized platinum with candidate propellants for resistojets. [Washington, DC]: National Aeronautics and Space Administration, 1985.

Whalen, Margaret V. Compatibility of grain-stabilized platinum with candidate propellants for resistojets. [Washington, DC]: National Aeronautics and Space Administration, 1985.

Yiming, Li, ed. Ye ti yun zai huo jian xi tong dian ci jian rong xing wen ji. Beijing Shi: Yu hang chu ban she, 2002.

Low power dc arcjet operation with hydrogen/nitrogen propellant mixtures. [Washington, DC]: National Aeronautics and Space Administration, 1986.

Center, NASA Glenn Research, ed. Advanced electric propulsion for space solar power satellites. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

M, Nelms R., Shepherd Michael T, and United States. National Aeronautics and Space Administration., eds. Design of a ZVS PWM inverter for a brushless DC motor in an EMA application. [Washington, DC: National Aeronautics and Space Administration, 1993.

Numerical simulation of cylindrical, self-field MPD thrusters with multiple propellants. [Washington, DC]: National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration., ed. Numerical simulation of cylindrical, self-field MPD thrusters with multiple propellants. [Washington, DC]: National Aeronautics and Space Administration, 1994.

J, Boyle Robert, McConnaughey H. V, United States. National Aeronautics and Space Administration., and United States. Army Aviation Research and Technology Activity., eds. Impact of ETO propellants on the aerothermodynamic analyses of propulsion components. [Washington, DC]: National Aeronautics and Space Administration, 1988.

Edwards, Thomas D. Implementation of three speckle reduction filters for solid propellant combustion holograms. 1986.

Redman, David N. Image analysis of solid propellant combustion holograms using an imageaction software package. 1986.

Shook, Marvin Philip. Computer-controlled image analysis of solid propellant combustion holograms using Quantimet 720 and a PDP-11. 1985.

Takeshi, Tachibana, and United States. National Aeronautics and Space Administration., eds. The Use of electrical discharge for ignition and control of combustion of solid propellants. Washington DC: National Aeronautics and Space Administration, 1987.

V, Whalen Margaret, Sovey J. S, and Lewis Research Center, eds. Performance and endurance tests of a multipropellant resistojet for space station auxiliary propulsion. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

McDonnell Douglas Astronautics Company--Houston Division. and United States. National Aeronautics and Space Administration., eds. Independent Orbiter assessment: Assessment of the electrical power generation/power reactant storage and distribution subsystem FMEA/CIL. Houston, Tex: McDonnell Douglas Astronautics Company, Houston Division, 1988.

Coaxial microwave electrothermal thruster performance in hydrogen: W. Richardson and J. Asmussen. [Washington, DC: National Aeronautics and Space Administration, 1994.