Advanced Space Propulsion (eBook)

Technologies, Missions, and Computer Modeling
Artikelnummer: 978-0-443-33810-6
Einband: Adobe Digital Editions
Verfügbarkeit: Download, sofort verfügbar (Link per E-Mail)
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PART I: ORBITS AND MISSIONS1. HISTORY2. SPACECRAFT MISSIONS3. MISSION ANALYSIS4. ORBIT THEORY5. STRAIGHT LINE TRAJECTORIES6. TRAJECTORY PLANNING AND OPTIMIZATIONPART II: POWER FOR PROPULSION SYSTEMS AND PROPULSION SOURCES7. CHEMICAL8. SOLAR9. NUCLEAR FISSION10. NUCLEAR FUSION11. POWER BEAMING12. SOLAR SAILS13. ELECTRIC POWER CONVERSIONPART III: PROPULSION MISSION CASE STUDIES14. DEEP SPACE 115. BEPICOLUMBO16. GEO SATELLITE STATIONKEEPING17. LEO ORBIT MAINTENANCEPART IV: PROPULSION FUTURE MISSIONS18. HUMAN MARS MISSION WITH NUCLEAR THERMAL19. ORBITAL MISSION TO URANUS20. TITAN FUSION POWERED AIRCRAFT21. MISSION TO MERCURY22. SOLAR GRAVITATIONAL LENS23. ALPHA CENTAURI ORBITER

PART I: ORBITS AND MISSIONS1. HISTORY2. SPACECRAFT MISSIONS3. MISSION ANALYSIS4. ORBIT THEORY5. STRAIGHT LINE TRAJECTORIES6. TRAJECTORY PLANNING AND OPTIMIZATIONPART II: POWER FOR PROPULSION SYSTEMS AND PROPULSION SOURCES7. CHEMICAL8. SOLAR9. NUCLEAR FISSION10. NUCLEAR FUSION11. POWER BEAMING12. SOLAR SAILS13. ELECTRIC POWER CONVERSIONPART III: PROPULSION MISSION CASE STUDIES14. DEEP SPACE 115. BEPICOLUMBO16. GEO SATELLITE STATIONKEEPING17. LEO ORBIT MAINTENANCEPART IV: PROPULSION FUTURE MISSIONS18. HUMAN MARS MISSION WITH NUCLEAR THERMAL19. ORBITAL MISSION TO URANUS20. TITAN FUSION POWERED AIRCRAFT21. MISSION TO MERCURY22. SOLAR GRAVITATIONAL LENS23. ALPHA CENTAURI ORBITER

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VerlagElsevier Science & Techn.
EinbandAdobe Digital Editions
Erscheinungsjahr2026
Seitenangabe700 S.
AusgabekennzeichenEnglisch
Masse65'725 KB
PlattformEPUB
AutorPaluszek EAA, Michael / Galea, Christopher A. / Mirdamadi BSE, Parisa / Mo, Joyce / Aboud, Layla Mohsen / Thomas, Stephanie J.

Über den Autor Michael Paluszek EAA

Michael Paluszek is the President of Princeton Satellite Systems, Inc. (PSS). He received a bachelor's degree in electrical engineering from the Massachusetts Institute of Technology (MIT) in 1976. He received a Master's and Masters and an Engineer's degree from MIT in Aeronautics and Astronautics in 1979. In 1992, Mr. Paluszek founded PSS in Plainsboro, New Jersey, to provide aerospace design services. He designed the control system and simulations for the Indostar-1 geosynchronous communications satellite, which launched in 1997, as well as a Mars Ascent Vehicle for a NASA RFP. He also designed a two-stage-to-orbit vehicle which uses a turbofan in the first stage for low-Mach numbers, and a ramjet with a hydrogen-fueled combustor for high-Mach flight. His current projects include a waverider hypersonic small package delivery aircraft and the Starfire fusion reactor for energy generation and space propulsion. Before founding PSS, Mr. Paluszek was an engineer at GE Astro Space in East Windsor, NJ. At GE, he designed the Global Geospace Sciences Polar despun platform control system and led the design of the GPS IIR attitude control system, the Inmarsat-3 attitude control systems, and the Mars Observer Delta-V control system. Mr. Paluszek flew communication satellites on over twelve satellite launches, including the GSTAR III recovery, the first transfer of a satellite to an operational orbit using electric thrusters. At Draper Laboratory, Mr. Paluszek worked on Space Shuttle and Space Station programs and on submarine navigation. His Space Station work included designing Control Moment Gyro-based attitude-control systems. He authored ``ADCS: Attitude Determination and Control Systems,'' published by Elsevier. Mr. Paluszek has also written numerous technical papers and has over a dozen U.S. Patents. He is also the lead co-author of ``MATLAB Recipes,'' ``MATLAB Machine Learning,'' ``MATLAB Machine Learning Recipes: A Problem-Solution Approach,'' ``Practical MATLAB Deep Learning Projects,'' and ``MATLAB Recipes Revised Edition,'' published by Apress.

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