Modern Engineering for Design of Liquid-Propellant Rocket EnginesFrom the component design, to the subsystem design, to the engine systems design, engine development and flight-vehicle application, this how-to text bridges the gap between basic physical and design principles and actual rocket-engine design as it's done in industry. |
Contents
CXCI | 203 |
CXCII | 204 |
CXCIII | 205 |
CXCIV | 207 |
CXCV | 212 |
CXCVI | 215 |
CXCVII | 217 |
CXCVIII | 218 |
XVIII | 16 |
XIX | 18 |
XXIV | 19 |
XXIX | 23 |
XXXI | 24 |
XXXIII | 25 |
XXXIV | 26 |
XXXV | 27 |
XXXVIII | 29 |
XLI | 32 |
XLII | 34 |
XLIV | 41 |
XLV | 44 |
XLVII | 45 |
XLVIII | 47 |
XLIX | 49 |
L | 53 |
LIII | 54 |
LIV | 55 |
LVII | 57 |
LX | 59 |
LXII | 60 |
LXV | 64 |
LXVI | 65 |
LXVII | 67 |
LXVIII | 68 |
LXX | 69 |
LXXIII | 71 |
LXXV | 72 |
LXXVI | 74 |
LXXVII | 75 |
LXXVIII | 79 |
LXXIX | 83 |
LXXX | 84 |
LXXXI | 85 |
LXXXII | 88 |
LXXXIII | 89 |
LXXXIV | 91 |
LXXXVI | 93 |
LXXXVIII | 96 |
LXXXIX | 98 |
XCI | 99 |
XCIII | 100 |
XCV | 101 |
XCVI | 103 |
XCVII | 104 |
C | 105 |
CI | 106 |
CIII | 107 |
CIV | 109 |
CVI | 110 |
CVII | 111 |
CVIII | 112 |
CX | 113 |
CXI | 114 |
CXII | 115 |
CXIII | 116 |
CXV | 117 |
CXVI | 118 |
CXVII | 119 |
CXVIII | 120 |
CXX | 121 |
CXXI | 126 |
CXXII | 127 |
CXXIII | 128 |
CXXIV | 129 |
CXXV | 130 |
CXXVII | 131 |
CXXXV | 132 |
CXL | 133 |
CXLII | 135 |
CXLVII | 136 |
CXLVIII | 139 |
CL | 140 |
CLI | 143 |
CLIII | 144 |
CLV | 146 |
CLVII | 147 |
CLIX | 148 |
CLXI | 149 |
CLXII | 152 |
CLXIII | 153 |
CLXIV | 155 |
CLXV | 157 |
CLXVI | 160 |
CLXVII | 162 |
CLXIX | 165 |
CLXXII | 175 |
CLXXIII | 179 |
CLXXV | 180 |
CLXXVI | 181 |
CLXXVII | 184 |
CLXXVIII | 186 |
CLXXIX | 187 |
CLXXX | 188 |
CLXXXI | 189 |
CLXXXII | 191 |
CLXXXIII | 192 |
CLXXXIV | 193 |
CLXXXVI | 194 |
CLXXXVIII | 195 |
CLXXXIX | 197 |
CXC | 199 |
CXCIX | 219 |
CC | 220 |
CCII | 222 |
CCIII | 225 |
CCV | 228 |
CCVI | 234 |
CCVII | 241 |
CCVIII | 242 |
CCIX | 244 |
CCX | 248 |
CCXI | 250 |
CCXII | 252 |
CCXIII | 256 |
CCXIV | 257 |
CCXV | 258 |
CCXVI | 261 |
CCXVII | 265 |
CCXVIII | 267 |
CCXIX | 268 |
CCXX | 273 |
CCXXI | 274 |
CCXXIV | 275 |
CCXXVII | 276 |
CCXXX | 277 |
CCXXXI | 278 |
CCXXXII | 279 |
CCXXXIII | 280 |
CCXXXIV | 282 |
CCXXXV | 285 |
CCXXXVI | 286 |
CCXXXIX | 287 |
CCXL | 288 |
CCXLII | 289 |
CCXLIII | 290 |
CCXLV | 291 |
CCXLVIII | 292 |
CCXLIX | 295 |
CCLI | 296 |
CCLIV | 297 |
CCLVI | 298 |
CCLVIII | 299 |
CCLX | 300 |
CCLXIII | 301 |
CCLXVI | 302 |
CCLXVIII | 303 |
CCLXX | 305 |
CCLXXII | 309 |
CCLXXIV | 311 |
CCLXXVIII | 312 |
CCLXXX | 314 |
CCLXXXI | 315 |
CCLXXXII | 317 |
CCLXXXIII | 321 |
CCLXXXIV | 325 |
CCLXXXV | 326 |
CCLXXXVI | 328 |
CCLXXXVII | 330 |
CCLXXXVIII | 332 |
CCXC | 335 |
CCXCII | 337 |
CCXCIII | 338 |
CCXCIV | 339 |
CCXCVI | 340 |
CCXCIX | 341 |
CCC | 342 |
CCCI | 345 |
CCCII | 346 |
CCCV | 348 |
CCCVI | 349 |
CCCVIII | 350 |
CCCXI | 351 |
CCCXII | 352 |
CCCXIII | 354 |
CCCXV | 355 |
CCCXVII | 356 |
CCCXVIII | 357 |
CCCXX | 359 |
CCCXXI | 360 |
CCCXXIII | 361 |
CCCXXIV | 363 |
CCCXXV | 364 |
CCCXXVII | 365 |
CCCXXVIII | 371 |
CCCXXXI | 372 |
CCCXXXIII | 373 |
CCCXXXIV | 374 |
CCCXXXV | 375 |
CCCXXXVII | 377 |
CCCXXXIX | 381 |
CCCXL | 383 |
CCCXLII | 384 |
CCCXLIII | 385 |
CCCXLVI | 386 |
CCCXLVIII | 388 |
CCCXLIX | 389 |
CCCL | 393 |
CCCLI | 399 |
| 405 | |
CCCLIII | 415 |
CCCLIV | 417 |
| 419 | |
CCCLVI | 427 |
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Common terms and phrases
A-4 Stage actuator alloys applications area ratio assembly axial bellows bipropellant blades chamber pressure characteristics coefficient combustion chamber combustor components configuration coolant cooling cryogenic diameter diaphragm duct dynamic effects efficiency elastomer engine system equations factor flange flow rate flowrate fluid ft/s fuel gas-generator cycle gases gimbal heat helium hydrogen hypergolic ignition impeller Inconel increase injection injector inlet installation ISBN joint lb/s leakage liquid loads material maximum mixture ratio nozzle NPSH O-ring operating orifice outlet Oxidizer parameters payload Pc)ns performance poppet pressure drop propellant tanks propulsion system psia pump radial regenerative cooling regulator reliability rocket engine rotor seal sensor shaft shown in Fig specific heat ratio specific impulse speed SSME Stage engine stress surface tank pressure Teflon temperature thermal throat thrust chamber thrust-chamber tion tube turbine turbopump Typical UDMH valve vane vehicle velocity wall weight welded


