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Relevant bibliographies by topics / Thrust specific impulse / Books

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Books on the topic 'Thrust specific impulse'

Author: Grafiati

Published: 2 June 2025

Last updated: 31 July 2025

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1

Williams, Craig Hamilton. An analytic approximation to very high specific impulse and specific power interplanetary space mission analysis. National Aeronautics and Space Administration, 1995.

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2

M, Kazaroff John, Pavli Albert J, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

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3

M, Kazaroff John, Pavli Albert J, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

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4

M, Kazaroff John, Pavli Albert J, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, eds. Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

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5

W, Haag Thomas, Manzella David H, and United States. National Aeronautics and Space Administration., eds. Operating characteristics of the Russian D-55 thruster with anode layer. National Aeronautics and Space Administration, 1994.

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6

United States. National Aeronautics and Space Administration., ed. The diagnostics of the external plasma for the plasma rocket: Final report, NASA Graduate Student Researchers Program, Johnson Space Center, contract number--NGT9-5. National Aeronautics and Space Administration, 1997.

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7

United States. National Aeronautics and Space Administration., ed. The diagnostics of the external plasma for the plasma rocket: Final report, NASA Graduate Student Researchers Program, Johnson Space Center, contract number--NGT9-5. National Aeronautics and Space Administration, 1997.

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8

N, Matossian J., and United States. National Aeronautics and Space Administration., eds. High-power ion thruster technology. National Aeronautics and Space Administration, 1996.

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9

N, Matossian J., and United States. National Aeronautics and Space Administration., eds. High-power ion thruster technology. National Aeronautics and Space Administration, 1996.

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10

N, Matossian J., and United States. National Aeronautics and Space Administration., eds. High power ion thruster technology. National Aeronautics and Space Administration, 1992.

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11

N, Matossian J., and United States. National Aeronautics and Space Administration., eds. High-power ion thruster technology. National Aeronautics and Space Administration, 1996.

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12

S, Sovey J., and United States. National Aeronautics and Space Administration., eds. The Evolutionary development of high specific impulse electric thruster technology. National Aeronautics and Space Administration, 1992.

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13

H, Berns Darren, and United States. National Aeronautics and Space Administration., eds. Performance of a low-power subsonic-arc-attachment arcjet thruster. NASA, 1993.

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14

H, Berns Darren, and United States. National Aeronautics and Space Administration., eds. Performance of a low-power subsonic-arc-attachment arcjet thruster. NASA, 1993.

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15

H, Berns Darren, and United States. National Aeronautics and Space Administration., eds. Performance of a low-power subsonic-arc-attachment arcjet thruster. NASA, 1993.

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16

An analytic approximation to very high specific impulse and specific power interplanetary space mission analysis. National Aeronautics and Space Administration, 1995.

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17

High-power ion thruster technology. National Aeronautics and Space Administration, 1996.

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18

Prussing, John E. Rocket Trajectories. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198811084.003.0003.

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Abstract:

rocket trajectories, including equations of motion are treated. High- and low-thrust engines are analysed, including constant-specific-impulse and variable-specific-impulse engines. The equation of motion of a spacecraft which is thrusting in a gravitational field determines its trajectory.

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19

Liquid Bismuth Propellant Management System for the Very High Specific Impulse Thruster with Anode Layer. Independently Published, 2020.

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20

Performance of a low-power subsonic-arc-attachment arcjet thruster. NASA, 1993.

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