History of Liquid Propellant Rocket EnginesAIAA, 2006 - 911 páginas This book, written by one of the foremost experts in rocket propulsion, gives an account of the liquid propellant rocket engine field over the last four-score and more years. It is the story about the technological advances that allowed progressive improvements in design, analysis, thrust magnitude, reliability, cost, and performance ; where and when those advances were made, including unique engines from the countries most important to this technology ; the groups, companies, or organizations of engineers, specialists, and dedicated people who made it happen ; and the different kinds of flight vehicles that have been propelled by liquid propellant rocket engines. It describes the early pioneers, amateur rocket societies, evolution of key hardware components, past investigations of different liquid propellants, reorganizations and mergers of key companies, and the principal areas of current and former applications. Both large pump-fed rocket engine and low thrust ensta gas-pressure-fed rocket engines with multiple thrusters are included. |
Conteúdo
I | 1 |
II | 5 |
III | 6 |
IV | 16 |
V | 23 |
VI | 25 |
VIII | 27 |
IX | 28 |
XXXIX | 359 |
XL | 404 |
XLI | 474 |
XLII | 491 |
XLIII | 510 |
XLIV | 531 |
XLV | 532 |
XLVI | 559 |
X | 29 |
XI | 32 |
XII | 33 |
XIII | 54 |
XIV | 74 |
XV | 108 |
XVI | 131 |
XVII | 147 |
XIX | 182 |
XX | 201 |
XXI | 218 |
XXII | 228 |
XXIII | 241 |
XXV | 247 |
XXVI | 271 |
XXVII | 276 |
XXVIII | 281 |
XXIX | 289 |
XXX | 293 |
XXXI | 303 |
XXXII | 307 |
XXXIV | 311 |
XXXV | 327 |
XXXVI | 346 |
XXXVII | 351 |
XXXVIII | 356 |
XLVII | 577 |
XLVIII | 585 |
XLIX | 629 |
L | 661 |
LI | 684 |
LII | 693 |
LIII | 698 |
LIV | 710 |
LV | 721 |
LVI | 725 |
LVII | 726 |
LVIII | 728 |
LIX | 737 |
LX | 738 |
LXI | 740 |
LXII | 754 |
LXIII | 763 |
LXIV | 769 |
LXV | 785 |
LXVI | 815 |
LXVII | 843 |
LXVIII | 865 |
LXIX | 881 |
LXX | 887 |
Termos e frases comuns
Aerojet AIAA Paper aircraft altitude Astronautics attitude control ballistic missile bipropellant Boeing Company booster CADB catalyst chamber pressure Chapter combustion chamber coolant cooling jacket copied with permission Courtesy Design Bureau developed early engine cycle experimental film cooling flight tested flown gear German gimbal Glushko Goddard heat hydrazine hydrogen peroxide hypergolic ignition impeller injection elements inlet JATO large LPRES lbf thrust LOX/kerosene LOX/LH₂ LPRE main engine maneuvers manifold mixture ratio monopropellant nitric acid nozzle-exit NPO Energomash NTO/UDMH operation orbit oxidizer payload pellant performance permission from Ref Personal communications pipe preburner propellant tanks Propulsion and Power regenerative cooling restart RFNA rocket engine Rocket Propulsion Rocketdyne Rocketdyne Propulsion second stage shaft shown in Fig small thrusters solid-propellant Soviet Union spacecraft specific impulse staged combustion cycle started storable propellants tank pressurization temperature throttling thrust chamber tubes turbine exhaust turbopump UDMH United upper stage wall warm gas
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Página 901 - Hunsaker Professor of Aeronautical Engineering at the Massachusetts Institute of Technology and has been on the faculty of the California Institute of Technology.