|
|
|
|
LEADER |
00000cam a2200000 i 4500 |
001 |
KNOVEL_ocn965197044 |
003 |
OCoLC |
005 |
20231027140348.0 |
006 |
m o d |
007 |
cr cnu---unuuu |
008 |
161205s2017 nju ob 001 0 eng d |
040 |
|
|
|a N$T
|b eng
|e rda
|e pn
|c N$T
|d YDX
|d UAB
|d MERER
|d OCLCQ
|d LIP
|d COO
|d UWW
|d NRC
|d BUF
|d CEF
|d RRP
|d ZCU
|d OCLCQ
|d UKOBU
|d UMI
|d OCLCF
|d VLB
|d K6U
|d CCO
|d LOA
|d COCUF
|d WRM
|d STF
|d VT2
|d AU@
|d WYU
|d LVT
|d ESU
|d UKAHL
|d OCLCQ
|d OCLCO
|d OCLCQ
|d OCLCO
|
019 |
|
|
|a 965479786
|a 965739063
|a 966396620
|a 967770943
|a 985460498
|a 1229061515
|
020 |
|
|
|a 9781118753880
|q (electronic bk.)
|
020 |
|
|
|a 1118753887
|q (electronic bk.)
|
020 |
|
|
|a 9781523110513
|
020 |
|
|
|a 1523110511
|
020 |
|
|
|a 1118753917
|
020 |
|
|
|a 9781118753910
|
020 |
|
|
|z 9781118753651
|
020 |
|
|
|z 1118753658
|
020 |
|
|
|z 9781118753910
|q (epub)
|
035 |
|
|
|a (OCoLC)965197044
|z (OCoLC)965479786
|z (OCoLC)965739063
|z (OCoLC)966396620
|z (OCoLC)967770943
|z (OCoLC)985460498
|z (OCoLC)1229061515
|
037 |
|
|
|a CL0500000854
|b Safari Books Online
|
050 |
|
4 |
|a TL782
|b .S8 2016eb
|
072 |
|
7 |
|a TEC
|x 009000
|2 bisacsh
|
082 |
0 |
4 |
|a 629.47/5
|2 23
|
049 |
|
|
|a UAMI
|
100 |
1 |
|
|a Sutton, George P.
|q (George Paul),
|d 1920-
|e author.
|
245 |
1 |
0 |
|a Rocket propulsion elements /
|c George P. Sutton, Oscar Biblarz.
|
250 |
|
|
|a Ninth edition.
|
264 |
|
1 |
|a Hoboken, New Jersey :
|b John Wiley & Sons Inc.,
|c [2017]
|
300 |
|
|
|a 1 online resource
|
336 |
|
|
|a text
|b txt
|2 rdacontent
|
337 |
|
|
|a computer
|b c
|2 rdamedia
|
338 |
|
|
|a online resource
|b cr
|2 rdacarrier
|
504 |
|
|
|a Includes bibliographical references and index.
|
588 |
0 |
|
|a Print version record.
|
505 |
0 |
|
|a Cover; Title Page; Copyright; Contents; Preface; Chapter 1: Classification; 1.1. Duct Jet Propulsion; 1.2. Rocket Propulsion; Chemical Rocket Propulsion; Combinations of Ducted Jet Engines and Rocket Engines; Nuclear Rocket Engines; Electric Rocket Propulsion; Other Rocket Propulsion Concepts; International Rocket Propulsion Effort; 1.3. Applications of Rocket Propulsion; Space Launch Vehicles; Spacecraft; Military and Other Applications; References; Chapter 2: Definitions and Fundamentals; 2.1. Definitions; 2.2. Thrust; 2.3. Exhaust Velocity; 2.4. Energy and Efficiencies.
|
505 |
8 |
|
|a 2.5. Multiple Propulsion Systems2.6. Typical Performance Values; 2.7. Variable Thrust; Symbols; Greek Letters; Problems; References; Chapter 3: Nozzle Theory and Thermodynamic Relations; 3.1. Ideal Rocket Propulsion Systems; 3.2. Summary of Thermodynamic Relations; 3.3. Isentropic Flow through Nozzles; Velocity; Nozzle Flow and Throat Condition; Thrust and Thrust Coefficient; Characteristic Velocity and Specific Impulse; Under- and Overexpanded Nozzles; Influence of Chamber Geometry; 3.4. Nozzle Configurations; Cone- and Bell-Shaped Nozzles; 3.5. Real Nozzles; Boundary Layers; Multiphase Flow.
|
505 |
8 |
|
|a Other Phenomena and LossesPerformance Correction Factors; Four Performance Parameters; 3.6. Nozzle Alignment; Symbols; Greek Letters; Subscripts; Problems; References; Chapter 4: Flight Performance; 4.1. Gravity-Free Drag-Free Space Flight; 4.2. Forces Acting on a Vehicle in the Atmosphere; 4.3. Basic Relations of Motion; 4.4. Space Flight; Elliptical Orbits; Deep Space; Perturbations; Mission Velocity; 4.5. Space Flight Maneuvers; Reaction Control System; 4.6. Effect of Propulsion System on Vehicle Performance; 4.7. Flight Vehicles; Multistage Vehicles; Stage Separation; Launch Vehicles.
|
505 |
8 |
|
|a 4.8. Military Missiles4.9. Flight Stability; Symbols; Greek Letters; Subscripts; Problems; References; Chapter 5: Chemical Rocket Propellant Performance Analysis; 5.1. Background and Fundamentals; 5.2. Analysis of Chamber or Motor Case Conditions; 5.3. Analysis of Nozzle Expansion Processes; 5.4. Computer-Assisted Analysis; 5.5. Results of Thermochemical Calculations; Greek Letters; Subscripts; Problems; References; Chapter 6: Liquid Propellant Rocket Engine Fundamentals; 6.1. Types of Propellants; 6.2. Propellant Tanks; 6.3. Propellant Feed Systems; Local Pressures and Flows.
|
505 |
8 |
|
|a 6.4. Gas Pressure Feed Systems6.5. Tank Pressurization; Factors Influencing the Required Mass of Pressurizing Gas; Simplified Analysis for the Mass of Pressurizing Gas; 6.6. Turbopump Feed Systems and Engine Cycles; Engine Cycles; 6.7. Rocket Engines for Maneuvering, Orbit Adjustments, or Attitude Control; 6.8. Engine Families; 6.9. Valves and Pipelines; 6.10. Engine Support Structure; Symbols; Subscripts; Problems; References; Chapter 7: Liquid Propellants; 7.1. Propellant Properties; Economic Factors; Performance of Propellants; Common Physical Hazards; Desirable Physical Properties.
|
520 |
|
|
|a Combining fundamental concepts with industry applications, this unique book provides a practical introduction to rocket propulsion principles, mechanisms, and design as applied to guided missiles, space flight, satellite flight, and more. --
|c Edited summary from book.
|
590 |
|
|
|a Knovel
|b ACADEMIC - Aerospace & Radar Technology
|
650 |
|
0 |
|a Rocket engines.
|
650 |
|
6 |
|a Moteurs-fusées.
|
650 |
|
7 |
|a TECHNOLOGY & ENGINEERING
|x Engineering (General)
|2 bisacsh
|
650 |
|
7 |
|a Rocket engines
|2 fast
|
700 |
1 |
|
|a Biblarz, Oscar,
|e author.
|
776 |
0 |
8 |
|i Print version:
|a Sutton, George P. (George Paul), 1920-
|t Rocket propulsion elements.
|b Ninth edition.
|d Hoboken, New Jersey : John Wiley & Sons Inc., [2016]
|z 9781118753651
|w (DLC) 2016031557
|w (OCoLC)953576462
|
856 |
4 |
0 |
|u https://appknovel.uam.elogim.com/kn/resources/kpRPEE001A/toc
|z Texto completo
|
938 |
|
|
|a Askews and Holts Library Services
|b ASKH
|n AH30555467
|
938 |
|
|
|a Askews and Holts Library Services
|b ASKH
|n AH30555466
|
938 |
|
|
|a EBSCOhost
|b EBSC
|n 1429756
|
938 |
|
|
|a YBP Library Services
|b YANK
|n 13287504
|
994 |
|
|
|a 92
|b IZTAP
|