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Books on the topic 'Roket simulation'

Author: Grafiati
Published: 28 May 2022
Last updated: 31 July 2025

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1

United States. National Aeronautics and Space Administration., ed. Solid rocket combustion simulator technology (using the hybrid rocket for simulation): Final report. University of Arizona, Engineering Experiment Station, College of Engineering and Mines, 1994.

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2

Hirshorn, Jessica. Rocket: A simulation on intercultural teamwork. Intercultural Press, 2010.

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3

Hirshorn, Jessica. Rocket: A simulation on intercultural teamwork. Intercultural Press, 2010.

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4

Hirshorn, Jessica. Rocket: A simulation on intercultural teamwork. Intercultural Press, 2010.

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5

Stuart, Thomas A. A study of ignition and simulation circuits for arcjet thrusters. U.S. National Aeronautics and Space Administration, 1991.

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6

Stuart, Thomas A. A study of ignition and simulation circuits for arcjet thrusters. U.S. National Aeronautics and Space Administration, 1991.

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7

D, Southwick R., and United States. National Aeronautics and Space Administration., eds. Large liquid rocket engine transient performance simulation system. Pratt & Whitney, 1989.

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8

D, Southwick R., and United States. National Aeronautics and Space Administration., eds. Large liquid rocket engine transient performance simulation system. United Technologies, Pratt & Whitney ; [Washington, DC, 1989.

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9

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Thermal stratification potential in rocket engine coolant channels. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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10

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Thermal stratification potential in rocket engine coolant channels. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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11

Alan, Palazzolo, and United States. National Aeronautics and Space Administration., eds. Enhanced simulation software for rocket turbopump, turbulent, annular liquid seals. National Aeronautics and Space Administration, 1994.

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12

D, Southwick R., and George C. Marshall Space Flight Center., eds. Large liquid rocket engine transient performance simulation system: Final report. United Technologies Corporation, Pratt & Whitney, Government Engine Business, 1991.

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13

P, Chen C., Ziebarth J. P, and University of Alabama. Dept. of Computer Science., eds. A combined Eulerian-volume of fraction-Lagrangian method for atomization simulation: Final report, contract no: NAS 8-38609 D.O. 56. University of Alabama, 1994.

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14

Sinibaldi, Edoardo. Implicit preconditioned numerical schemes for the simulation of three-dimensional barotropic flows. Edizioni della Normale, 2007.

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15

United States. National Aeronautics and Space Administration., ed. An RL10A-3-3A rocket engine model using the rocket engine transient simulator (ROCETS) software. National Aeronautics and Space Administration, 1993.

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16

United States. National Aeronautics and Space Administration., ed. An RL10A-3-3A rocket engine model using the rocket engine transient simulator (ROCETS) software. National Aeronautics and Space Administration, 1993.

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17

D, Smith S., Myruski Brian L, and United States. National Aeronautics and Space Administration., eds. Radiation from advanced solid rocket motor plumes. SECA, Inc., 1994.

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18

D, Smith S., Myruski Brian L, and United States. National Aeronautics and Space Administration., eds. Radiation from advanced solid rocket motor plumes. SECA, Inc., 1994.

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19

M, Ingels Franklin, and United States. National Aeronautics and Space Administration., eds. Space lab system analysis: Interim final report, October 1987 - October 1988. Mississippi State University, Electrical Engineering Dept., 1988.

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20

Rocker, M. Modeling on nonacoustic combustion instability in simulations of hybrid motor tests. National Aeronautics and Space Administration, Marshall Space Flight Center, 2000.

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21

Buckley, P. L. A simulator for a hydrocarbon ramrocket fuel gas generator - first phase development. Aeronautical Research Laboratory, 1989.

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22

Hamed, A. Probabilistic modeling for simulation of aerodynamic uncertainties in propulsion systems. National Aeronautics and Space Administration, 1989.

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23

Thomas, Tomsik, Veres Joseph P, and United States. National Aeronautics and Space Administration., eds. RL10A-3-3A rocket engine modeling project. National Aeronautics and Space Administration, 1997.

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24

Thomas, Tomsik, Veres Joseph P, and United States. National Aeronautics and Space Administration., eds. RL10A-3-3A rocket engine modeling project. National Aeronautics and Space Administration, 1997.

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25

Thomas, Tomsik, Veres Joseph P, and United States. National Aeronautics and Space Administration., eds. RL10A-3-3A rocket engine modeling project. National Aeronautics and Space Administration, 1997.

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26

Scott, McRae D., Bond Ryan B, and NASA Glenn Research Center, eds. Three dimensional numerical simulation of rocket-based combined-cycle engine response during mode transition events. National Aeronautics and Space Administration, Glenn Research Center, 2003.

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27

1950-, Alvarez Araya Oscar, and United States. National Aeronautics and Space Administration., eds. Laboratory simulation of the effect of rocket thrust on a precessing space vehicle: Final report. University of California, Los Angeles, Mechanical, Aerospace, and Nuclear Engineering Dept., 1990.

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28

United States. National Aeronautics and Space Administration., ed. Parallelization of Rocket Engine Simulator Software (PRESS): Research summary report : grant number: NAG3-1792; grant period: 3 years [October 19, 1995-October 18, 1998]. National Aeronautics and Space Administration, 1997.

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29

Center, NASA Glenn Research, ed. Finite element simulation of a space shuttle solid rocket booster aft skirt splashdown using an arbitrary Lagrangian-Eulerian approach. NASA Glenn Research Center, 2003.

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30

K, Lu Frank, and Marren Dan E, eds. Advanced hypersonic test facilities. American Institute of Aeronautics and Astronautics, 2002.

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31

Paul, Schallhorn, and United States. National Aeronautics and Space Administration., eds. Flow simulation in secondary flow passages of a rocket engine turbopump: Draft paper for 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, July 13-15, 1998, Cleveland, Ohio. National Aeronautics and Space Administration, 1998.

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32

J, Breisacher Kevin, and United States. National Aeronautics and Space Administration., eds. A comparison of analytical results for 20 K LOX/hydrogen instabilities. NASA, 1990.

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33

J, Breisacher Kevin, and United States. National Aeronautics and Space Administration., eds. A comparison of analytical results for 20 K LOX/hydrogen instabilities. NASA, 1990.

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34

Ronnie, Francis, Wells Eugene M, bd Systems Inc, and United States. National Aeronautics and Space Administration., eds. Final report for research study entitled "Performance evaluation of the Gravity Probe B design": Contract number NAS8-40618. National Aeronautics and Space Administration, 1996.

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35

Ronnie, Francis, Wells Eugene M, bd Systems Inc, and United States. National Aeronautics and Space Administration., eds. Final report for research study entitled "Performance evaluation of the Gravity Probe B design": Contract number NAS8-40618. National Aeronautics and Space Administration, 1996.

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36

Paul, Schallhorn, and United States. National Aeronautics and Space Administration., eds. Flow simulation in secondary flow passages of a rocket engine turbopump: Draft paper for 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, July 13-15, 1998, Cleveland, Ohio. National Aeronautics and Space Administration, 1998.

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37

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

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38

National Aeronautics and Space Administration (NASA) Staff. Nuclear Thermal Rocket Simulation in Npss. Independently Published, 2019.

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39

Wang, Zhen-Guo. Internal Combustion Processes of Liquid Rocket Engines: Modeling and Numerical Simulations. Wiley & Sons, Limited, John, 2016.

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40

Wang, Zhen-Guo. Internal Combustion Processes of Liquid Rocket Engines: Modeling and Numerical Simulations. Wiley & Sons, Incorporated, John, 2016.

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41

Wang, Zhen-Guo. Internal Combustion Processes of Liquid Rocket Engines: Modeling and Numerical Simulations. Wiley & Sons, Incorporated, John, 2016.

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42

Wang, Zhen-Guo. Internal Combustion Processes of Liquid Rocket Engines: Modeling and Numerical Simulations. Wiley & Sons, Limited, John, 2016.

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43

National Aeronautics and Space Administration (NASA) Staff. Numerical Simulation of Film-Cooled Ablative Rocket Nozzles. Independently Published, 2018.

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44

National Aeronautics and Space Administration (NASA) Staff. Parallelization of Rocket Engine Simulator Software (Press). Independently Published, 2018.

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45

Kratt, Aaron T. Numerical simulation of the ejector flowfield in a ram rocket engine with multiple rockets. 2004.

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46

National Aeronautics and Space Administration and NASA. Gas Mixtures for Dynamic Simulation of Rocket Exhaust Jets: November 23 1965. Independently Published, 2022.

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47

An RL10A-3-3A rocket engine model using the rocket engine transient simulator (ROCETS) software. National Aeronautics and Space Administration, 1993.

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48

National Aeronautics and Space Administration (NASA) Staff. Laboratory Simulation of the Effect of Rocket Thrust on a Precessing Space Vehicle. Independently Published, 2018.

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49

National Aeronautics and Space Administration (NASA) Staff. Theoretical Tools and Software for Modeling, Simulation and Control Design of Rocket Test Facilities. Independently Published, 2018.

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50

RL10A-3-3A rocket engine modeling project. National Aeronautics and Space Administration, 1997.

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