SMAD

Recommendations

Info

xii List of Authors List of Authors xiii Ronald A. Madler. Associate Professor, Embry-Riddle Aeronautical University, Prescott, Arizona. Ph.D., M.S., B.S. (Aerospace Engineering Sciences), University of Colorado, Boulder. Section 21.2-Drbital Debris-A Space Hazard. James R. McCandless. Manager (Retired), Stress Analysis, Space Systems, Lockheed Martin Astronautics, Denver, Colorado. B.S. (ArchitecturaI Engineering), University of Texas. Section 11.6-Structures and Mechanisms. Joseph K. McDermott. Engineering Manager, Lockheed Martin Astronautics Group, Denver, Colorado. M.E. (Engineering Management), University of Colorado; B.S. (Chemistry), Loras College. Section 11.4-Power. Darren S. McKnight. Vice President, Titan Research and Technology, Reston, Virginia. Ph.D. (Aerospace Engineering), University of Colorado; M.S. (Mechanical Engineering), University of New Mexico; B.S. (Engineering), U.S. Air Force Academy. Section 21.2-Orbital Debris-A Space Hazard. Wade Molnau. Manufacturing Manager, Motorola Systems Solutions Group, Space Services and Systems Division, Scottsdale, Arizona. Ph.D., M.S., B.S. (Industrial Engineering), Arizona State University. Section 19.1- DeSigning Space Systems/or Manu/acturability. Paul Nordin. NASAlTDRS Resident Office Manager at Hughes Space and Communications, EI Segundo, California, employed by The Boeing Company, Seabrook, MD. Ph.D .• M.A., B.A., (Nuclear Physics). University of California, Berkeley. Section S.2-Hardness and Survivability Requirements. Jean Olivieri. Teledesic Bus Production Manager. Motorola Advanced Systems Division, Chandler, Arizona. M.S .• B.S. (Industrial Engineering), Arizona State University. Section 19.1-Designing Space Systems for Manufacturability. Wes Ousley. Head, Thermal Engineering Branch, NASA Goddard Space Flight Center, Greenbelt, Maryland. B.S. (Mechanical Engineering), University of Maryland. Section Il.S-Thermal. Craig H. Pollock. Space Systems Engineer (Onboard Processing Design Integration and Operations Engineering), TRW Space and Defense Sector, Redondo Beach California. M.A. (Mathematics), California State University, Long Beach; B.S. (physics and Mathematics), University of New Mexico. Chapter 16-Spacecraft Computer Systems. Robert C. Prager. Engineering Specialist, The Aerospace Corporation, El Segundo, California. MS. (Engineering), University of California, Berkeley. B.S. (Engineering), Princeton University. Section 1l.5-Thermal. Emery I. Reeves. Shriever Chair Professor of Space Systems Engineering, U.S. Air Force Academy, Colorado Springs, Colorado. M.S. (Electrical Engineering), ':1assachusetts Institute of Technology; B.E. (Electrical Engineering), Yale Univer ~Ity. Chapter IO-Spacecraft Design and Sizing, Chapter 12-Spacecraft Manu/acure and Test. Richard P. Reinert. Staff Consultant, Spacecraft and Mission Design Division, Ball Aerospace Systems, Boulder, Colorado. B.S: (~eronautica1 ~ngi~eering), Massachusetts Institute of Technology. Chapter 2-Mr.sszon Charactenzat;.on. Robert L. Sackheim. Deputy Director, Propulsion Technology and. Fluid ~ec~cs Center, .TRW, Inc., Redondo Beach, California. M.S., B.S. (ChelDlca1 Engmeenng) Columbia University. Chapter 17-Space Propulsion Systems. Thomas P. Sarafin. Co~ultantlPresident, Instar Engineering and .Co~ting, ~c., Littleton, Colorado. B.S. (Civil Engineering), Ohio State Umverslty. Section 11.6-Structures and Mechanisms. Michael Schulz. Senior Scientist, Lockheed Martin Advanced Technology Center. Palo Alto, California. Ph.D. (physics),lVIassachusetts Institute of.Technology; B.S. (physics), Michigan State University. Section S.l-The Space EnVIronment. Cbad Spalt. Production Technical Lead, MotoR?la Satellite Comm~catio~ ~up, Mobile Satellite Systems Division, Chandler, Arizona. M.S. (Industrial EngmeerIng), Arizona State University; B.S. (Mechanical Engineering Technology), So~~ern Dlinois University. Section 19. I-Designing Space Systems/or Manufacturabillty. Gael F. Sqw"hb. Director for TeleCommunications and Mission Operations: Jet Propulsion Laboratory, Pasadena, California. M.S. (Systems Management), Umversity of Southern California; B.S. (physics), Harvey Mudd College. Chapter 14--Mission Operations Charles Teixeira. Chief, Systems Definition Branch, L.B. Jo~n Space Ce~ter, NASA, Houston, Texas. M.S. (Mechanical Engineering), LoUiSiana State Umversity; B.S. (Aeronautical Engineering), New York University. Chapter IS-Launch Systems. Alan C. Tribble. Manager, Applications Development, ~orma~on ~echnology: Rockwell Collins, Cedar Rapids, Iowa. Ph.D., M.S., (PhYSICS), Um~erslty of Iowa, B.S. (physics), University of Arkansas. Section S.l-The Space EnvIronment. A. L. Vampola. Consultant, Space Environment Eff~ts, Vista, Ca!ifornia. ~h.D., M.S. (physics), St Louis University; B.S. (Mathematics and PhYSICS), Creighton University, Nebraska. Section S.l-The Space Environment. R. L. Walterscheid. Senior Scientist, Space Sciences Department, Space. and Environment Technology Center, The Aerospace Corporation, EI Segundo, California. PhD. (Atmospheric Sciences), University of California, ~ Ang~les; .M.S. (Meteorology). University of California, Los Ang~les; A.~. (Phrslcs), ~mverslty of California, Berkeley; B.S. (Meteorology), UniVersity of WisconsIn. Section S.l-The Space Environment. Stanley I. Weiss. Visiting Professor, Massachusetts ~tute .of Technology and University of California Davis; Formerly Corporate ~ En1?neenng. an? VP Research and Development, Lockheed Corporation; PhD., ~mverslty of ~~OIS; M.s., B.S .• Renesselaer Polytechnic Institute. Chapter 4--RequJrements Definttton.
xiv List of Authors List of Authors xv James R. Wertz. President, Microcosm, Inc., Torrance, California. Ph.D. (Relativity & Cosmology), University of Texas, Austin; M.S. (Administration of Science and Technology), George Washington University; S.B. (physics), Massachusetts Institute of Technology. Editor; Chapter I-The Space Mission Analysis and Design Process; Chapter 2-Mission Characterization; Chapter 3-Mission Evaluation; Chapter 5-Space Mission Geometry; Chapter 7-0rbit and ConsteUation Design; Section S.I-The Space Environment; Section 1l.7--Guidance and Navigation; Chapter 2~Applying the Space Mission Analysis and Design Process; Appendix E-Universal Time and Julian Dates. Gary G. Whitworth. Senior Engineer (Retired), Applied Physics Laboratory, Johns Hopkins University, Laurel, Maryland. B.S. (Electrical Engineering), University of Tennessee. Chapter 15-Ground System Design and Sizing. Michael S. Williams. Vice President, Personal SATCOM Systems, Lockheed Martin Global Telecommunications, Reston, VA. M.S. (Electrical Engineering), University of Pennsylvania; M.B.A. (Statistics/Operations Research), Temple University; B.S. (Physics), St Joseph's University. Chapter 4-Requirements Definition. William B. Wirln. General Manager, Wirin & Associates. 1.D. (University of Southern California School of Law); B.A. (political Science), Occidental College. Section 21.1-Law and Policy Considerations. Robert E. Wong. Manager, Economic Analysis, TRW Systems Engineering and Development Division. TRW, Inc., Redondo Beach, California. PhD. (Economics), University of Southern California; M.S. (Mathematics), University of Southern California; M.A. (Economics), University of Southern California; B.S. (Physics), Iowa State University. Chapter 2O--Cost Modeling. Sidney Zafran. Program Manager, TRW, Inc., Redondo Beach, California. B.S. (Mechanical Engineering), Massachusetts Institute of Technology. Chapter 17- Space Propulsion Systems. <strong>SMAD</strong> I, ll, and m Authors The third edition is the end result of a substantial effort by the authors of all the <strong>SMAD</strong> editions. Consequently, we would like to acknowledge and express our thanks to alI of the authors who have contributed to this series: Henry Apgar David A. Bearden Robert Bell Richard T. Berget J. B. Blake James E. Boatwright Daryl G. Boden William R. Britton Robert F. Brodsky John B. Carraway Bruce Chesley Arthur Chomas John T. Collins Richard S. Davies Simon D. Dawson Fred 1. Dietrich Peter G. Doukas Neal Ely John S. Etemo Rick Fleeter John R. Ford, Jr. Martin E.B. France . David G. Gilmore Steven Glaseman D.J.Gorney EricW.Grob L. Jane Hansen Brian E. Hardt Herbert Hecht Robert W. Hosken Douglas Kirkpatrick Malcolm K. Kong H. C. Koons Wiley J. Larson Joseph P. Loftus, Jr. Reinhold Lutz Ronald A. Madler Fr~ois Martel James R. McCandless Joseph K. McDermott Darren S. McKnight Robert K. McMor4ie Wade Molnau Ralph L. Mueller David Negron, Jr. Paul Nordin Thomas P. O'Brien Jean Olivieri Wes Ousley Aniceto Panetti Craig H. Pollock Robert C. Prager Emery I. Reeves Richard P. Reinert Robert L. Sackheim Thomas P. Sarafin Michael Schulz ChadSpalt Gael F. Squibb Charles Teixeira Merlin E. Thimlar Alan C. Tribble Tim Tumer A. L. Vampola R. L. Walterscheid Richard Warner . Stanley I. Weiss James R. Wertz Gary G. Whitworth Michael S. Williams William B. Wirin Robert S. Wolf RobertE. Wong Sidney Zafran Robert O. Zennuehlen Harold F. Zimbelman
Page 1 and 2: THE SPACE TECHNOLOGY LmRARY Publish
Page 4 and 5: vill Table of Contents 21. 22. 23.
Page 8 and 9: 1 I Preface xvii Preface .Space. Mi
Page 10 and 11: Chapter 1 The Space Mission Analysi
Page 12 and 13: 4 The Space Mission Analysis and De
Page 14 and 15: 8 The Space Mission Analysis and De
Page 16 and 17: 12 The Space Mission Analysis and D
Page 18 and 19: -----------------------------------
Page 20 and 21: 20 Mission Characterization 2.1 Ste
Page 22 and 23: 24 Mission Characterization 2.1 2.1
Page 24 and 25: -----------------------------------
Page 26 and 27: 32 MIssion . Cbaracterlzation 2.2 S
Page 28 and 29: ---------------------------- - 36 M
Page 34 and 35: 48 Mission Evaluation 3.1 ing ~ana?
Page 36 and 37: 52 Mission Evaluation 3.2 3.2 Missi
Page 38 and 39: Mission Evaluation 3.2 document and
Page 40 and 41: 60 Mission Evaluation 3.3 3.3 Step
Page 46 and 47: 72 Mission Evaluation 3.4 requireme
Page 48 and 49: 76 Requirements Definition 4.1 requ
Page 50 and 51: 80 Requirements DefiDition 4.2 matr
Page 52 and 53: 84 Requirements Definition 4.2 4.2
Page 54 and 55: 88 Requirements Definition 4.2 Requ
Page 56 and 57:
Requirements De6oitiOD 4.3 4.4 Summ
Page 58 and 59:
96 Space Mission Geometry space mis
Page 60 and 61:
100 Space Mission Geometry ,,* , *
Page 62 and 63:
104 Space Mission Geometry 5.1 5.1
Page 64 and 65:
188 Space Mission Geometry 5.1 is t
Page 66 and 67:
112 Space Mission Geometry 5.2 Eart
Page 68 and 69:
116 Space Mission Geometry 5,2 The
Page 70 and 71:
Page 72 and 73:
Page 74 and 75:
Page 76 and 77:
132 Introdnction to Astrodynamles 6
Page 78 and 79:
136 Introduction to Astrodynamics i
Page 80 and 81:
140 Introduction to Astrodymmdcs 6.
Page 82 and 83:
144 Introduction to Astrodynamics T
Page 84 and 85:
148 Introdnction to Astrodynamics 6
Page 86 and 87:
152 Introduction to Astrodynamics 6
Page 88 and 89:
156 Introduction to Astrodynamlcs 6
Page 90 and 91:
160 Orbit and CODSteDatiOD Design 7
Page 92 and 93:
164 Orbit and CoDSteJlation Design
Page 94 and 95:
168 Orbit and CoDStellation Design
Page 96 and 97:
172 Orbit and ConsteDation Design 7
Page 98 and 99:
176 Orbit and Constellation Design
Page 100 and 101:
Page 102 and 103:
Page 104 and 105:
Page 106 and 107:
192 , Orbit and ConsteDation Design
Page 108 and 109:
Page 110 and 111:
200 Orbit and ConsteDadon Design 7.
Page 112 and 113:
204 The Space Environment and Survi
Page 114 and 115:
Page 116 and 117:
212 The Space En'Yironment.and Surv
Page 118 and 119:
Page 120 and 121:
Page 122 and 123:
Page 124 and 125:
Page 126 and 127:
Page 128 and 129:
The Space Environment and Survivabi
Page 130 and 131:
Page 132 and 133:
244 Space Payload Design and Sizing
Page 134 and 135:
Page 136 and 137:
Page 138 and 139:
Page 140 and 141:
Page 142 and 143:
Page 144 and 145:
Page 146 and 147:
272 Space Payload Design and SJzing
Page 148 and 149:
Page 150 and 151:
280 Space Payload Design and SiziDg
Page 152 and 153:
Page 154 and 155:
Page 156 and 157:
Page 158 and 159:
Page 160 and 161:
Page 162 and 163:
304 Spacecraft Design and Sizing lo
Page 164 and 165:
308 Spacecraft Design and Sizing 10
Page 166 and 167:
Page 168 and 169:
Page 170 and 171:
Page 172 and 173:
324 Spaeecraft Design and Sizing 1D
Page 174 and 175:
Page 176 and 177:
Page 178 and 179:
Page 180 and 181:
Page 182 and 183:
Page 184 and 185:
Page 186 and 187:
Page 188 and 189:
356 Spacecraft Subsystems 11.1 TABL
Page 190 and 191:
Spacecraft Subsystems 11.1 H.I Atti
Page 192 and 193:
364 spaceeraft Subsystems 11.1 TABL
Page 194 and 195:
368 Spacecraft Subsystems 11.1 11.1
Page 196 and 197:
372 Spacecraft Snbsystems 11.1 11.1
Page 198 and 199:
Page 200 and 201:
380 spacecraft Subsystems 11.1 11.2
Page 202 and 203:
384 Spacecraft Subsystems 11.2 vehi
Page 204 and 205:
Page 206 and 207:
392 UpDnk Composlta Signal RF CarrI
Page 208 and 209:
Page 210 and 211:
Page 212 and 213:
, I : ,i I I 404 Spacecraft Subsyst
Page 214 and 215:
Page 216 and 217:
I' 412 Spacecraft Subsystems 11.4 P
Page 218 and 219:
Page 220 and 221:
I~ ~ !~ : ~I' !, : , ' 420 Spacecra
Page 222 and 223:
I I! i 424 1.0 0.8 ~ 0.6 :!!. ! 0.4
Page 224 and 225:
428 Spacecraft Subsystems 11.s 11.5
Page 226 and 227:
Page 228 and 229:
436 Spacecraft Subsystems 11.s TABL
Page 230 and 231:
440 Spacecraft Subsystems 11.s Most
Page 232 and 233:
Page 234 and 235:
1 I ! 448 Spacecraft Subsystems 11.
Page 236 and 237:
452 Spacecraft Subsystems 11.5 U.5
Page 238 and 239:
456 Spacecraft Subsystems U.s 11.5
Page 240 and 241:
Spacecraft Subsystems 11.6 support
Page 242 and 243:
Page 244 and 245:
Page 246 and 247:
472 Spacecraft Subsystems 11.6 p 11
Page 248 and 249:
476 spaceeraft Subsystems 11.6 stru
Page 250 and 251:
480 Spacecraft Subsystems 1l.6 -e-
Page 252 and 253:
484 spacecraft Subsystems 11.6 11.6
Page 254 and 255:
488 Spacecraft Subsystems 1l.6 It.6
Page 256 and 257:
, ! 492 Spacecraft Subsystems TABLE
Page 258 and 259:
Page 260 and 261:
500 Spaceeraft Subsystems 11.7 11.7
Page 262 and 263:
Page 264 and 265:
508 Spacecraft Subsystems 11.7 Orbi
Page 266 and 267:
512 Spacecraft Subsystems 11.7 done
Page 268 and 269:
516 . Spacecraft Subsystems Referen
Page 270 and 271:
520 Spacecraft Manufacture and Test
Page 272 and 273:
Page 274 and 275:
t! 528 Spacecraft Manufacture and T
Page 276 and 277:
Page 278 and 279:
I 536 Communications Architecture 1
Page 280 and 281:
S40 Communications Architecture 13.
Page 282 and 283:
544 Communications Architecture 13.
Page 284 and 285:
548 Communications Architecture 13,
Page 286 and 287:
Page 288 and 289:
Page 290 and 291:
Page 292 and 293:
I : 564 Communications Architecture
Page 294 and 295:
:1 I~ :i! 568 Communications Archit
Page 296 and 297:
Page 298 and 299:
576 Communications An:hiteeture 13.
Page 300 and 301:
Page 302 and 303:
Page 304 and 305:
11 I" 588 Mission Operations 589 10
Page 306 and 307:
I I , , i 592 Mission Operations 14
Page 308 and 309:
S!J6 Mission Operations 14.1 • Wh
Page 310 and 311:
600 MIssion Operations 14.2 Step 12
Page 312 and 313:
604 Mission Operations 14.2 14.2 Ov
Page 314 and 315:
,!I 608 Mission Operations 14.2 eng
Page 316 and 317:
612 Mission Operations 14.3 14.3 Es
Page 318 and 319:
616 Mission Operations 14.4 14.4 Au
Page 320 and 321:
620 Mission Operations Squibb, Gael
Page 322 and 323:
624 Ground System Design and Sizing
Page 324 and 325:
~ ' 'I 1,1 IJ' i 628 Ground System
Page 326 and 327:
Page 328 and 329:
Ground System Design and Sizing 15.
Page 330 and 331:
Page 332 and 333:
644 Ground System Design and sizing
Page 334 and 335:
648 Spacecraft Computer Systems 16.
Page 336 and 337:
Page 338 and 339:
I' , ', 6S6 Spacecraft Computer Sys
Page 340 and 341:
Spacecraft Computer Systems 16.2 de
Page 342 and 343:
I , Spacecraft Computer Systems 16.
Page 344 and 345:
6fi8 Spacecraft Computer Systems 16
Page 346 and 347:
Page 348 and 349:
Page 350 and 351:
Ii 680 Spacecraft Computer Systems
Page 352 and 353:
Page 354 and 355:
688 Space Propulsion Systems 17.2 1
Page 356 and 357:
Page 358 and 359:
Page 360 and 361:
700 Space PropoJsion Systems - ....
Page 362 and 363:
704 Space Propulsion Systems ':1 20
Page 364 and 365:
I • I i i 708 Space Propulsion Sy
Page 366 and 367:
Page 368 and 369:
j ....!:. E ~ I ~ I ! . I I 716 Spa
Page 370 and 371:
720 Launch Systems 18.1 18.1 Basic
Page 372 and 373:
I I'. :( 724 Launch Systems 18,,2 i
Page 374 and 375:
~ "I, , I I j I d 1 728 Launch Syst
Page 376 and 377:
732 Launch Systems but the upper st
Page 378 and 379:
736 Launch Systems 18.3 18.3 Determ
Page 380 and 381:
. 740 TABLE 18-8. Vehicle T340nUS L
Page 382 and 383:
744 Launch Systems Pegasus Payl~ad
Page 384 and 385:
748 Space Manufacturing and ReHabil
Page 386 and 387:
~i Ii 752 Space ManufacturiJJg and
Page 388 and 389:
756 Space Manufacturing and Reliabi
Page 390 and 391:
Page 392 and 393:
764 Space Manufacturing and ReHabll
Page 394 and 395:
768 Space Manufacturing and ReHabDi
Page 396 and 397:
772 Space Manufacturing and ReJiabi
Page 398 and 399:
Page 400 and 401:
I '" ! I ~ 780 Space Manufacturing
Page 402 and 403:
;: j beginning of the process so th
Page 404 and 405:
lf I' f I II !, 788 Cost Modeling 2
Page 406 and 407:
792 Cost ModeHng 20.2 TABLE 20-2. P
Page 408 and 409:
II' 1 II I I :f, :1:, 796 Cost Mode
Page 410 and 411:
11' 1'1 800 Cost Modeling 20.3 20.3
Page 412 and 413:
804 Cost ModeJing 20.4 20.4 Other T
Page 414 and 415:
808 CostModeJiug 20.4 20.4 Other To
Page 416 and 417:
11 812 Cost ModeHng 2O.s TABLE 20-1
Page 418 and 419:
816 Cost Modeling 20.5 20.5 FireSat
Page 420 and 421:
820 Cost Modeling Wright, T. P. 193
Page 422 and 423:
824 Limits on Mission Design 21.1 a
Page 424 and 425:
828 Limits on Mission Design 21.1 t
Page 426 and 427:
i ,I I' , I 832 Limits on Mission D
Page 428 and 429:
- 836 Limits on Mission Design 21.1
Page 430 and 431:
840 Limits on Mission Design 21.2 T
Page 432 and 433:
844 Limits on Mission Design 21.2 o
Page 434 and 435:
848 Limits on Mission Design 21.2 T
Page 436 and 437:
852 Umits on Mission Design Yeomans
Page 438 and 439:
856 Design of Low-Cost Spacecraft 8
Page 440 and 441:
860 Design of Low-Cost Spacecraft s
Page 442 and 443:
Page 444 and 445:
Design of Low-Cost Spacecraft 22.2
Page 446 and 447:
872 Design ofLow-Cost Spacecraft 22
Page 448 and 449:
Page 450 and 451:
880 Design of Low -Cost Spacecraft
Page 452 and 453:
884 Applying the Space Mission Anal
Page 454 and 455:
888 Applying the Space Mission Anal
Page 456 and 457:
Applying the Space Mission Analysis
Page 458 and 459:
896 Appendix A TABLE A-2. Mass DIst
Page 460 and 461:
900 AppendixB Astronautical and Ast
Page 462 and 463:
Spherical Geometry 905 AppendixD .
Page 464 and 465:
908 AppendixD Spherieal Geometry in
Page 466 and 467:
912 AppendixD TABLE 0-9. Geometric
Page 468 and 469:
916 AppendixE, Universal Time and J
Page 470 and 471:
920 AppenttixF Units and Conversion
Page 472 and 473:
924 AppendixF Units and Conversion
Page 474 and 475:
Index ~sIgJDa dfSign process 746-74
Page 476 and 477:
932 Index Index 933 angular impulse
Page 478 and 479:
936 Index Index 937 Component Confi
Page 480 and 481:
Index Index 941 Disposal of spacecr
Page 482 and 483:
944 Index Index 945 miniature satel
Page 484 and 485:
i- 948 Index Index 949 design of 69
Page 486 and 487:
T I 952 Index Index 953 Loaded weig
Page 488 and 489:
956 Index 1 I • Index 957 NASA (S
Page 490 and 491:
T I 960 Index Index 961 representat
Page 492 and 493:
964 Index Index 965 scatterometers
Page 494 and 495:
968 Index Index 969 Solar sail Soli
Page 496 and 497:
972 Index Index 973 System noise te
Page 498 and 499:
976 Inde;t from nuclear explosion f
Page 500 and 501:
Exp~tion of Earth Satellite Paramet
Page 502 and 503:
------------- -------- Earth Satell
show all

SMAD

You also want an ePaper? Increase the reach of your titles

Delete template?

Save as template?