Volume VI Evaluation Data Book - National Space Society · 0180-22876-6 NAS9-15196 ORL T-1346...

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/' 0180-22876-6 NAS9-15196 ORL T-1346 OROMA-664T LINE ITEM 3 Volume VI Evaluation Data Book G3'/15 C19497 SYSTEM DEFINITION STUDY PART//

Transcript of Volume VI Evaluation Data Book - National Space Society · 0180-22876-6 NAS9-15196 ORL T-1346...

  • / '

    0180-22876-6

    NAS9-15196 ORL T-1346 OROMA-664T LINE ITEM 3

    Volume VI Evaluation Data Book

    ~1nclas

    G3'/15 C19497

    SYSTEM DEFINITION STUDY PART//

  • Dl80-2287U

    CONTRACT NAS9·15196 OF>:. T-t346 OROMA-664T LINE ITEM3

    Solar Power Satellite SYSTEM DEFl!.''TION STUDY

    PART/I

    VOLU~IE VI

    EVALUATION DATA BOOK

    D 18~228i6-6 DECEMBER J 9n

    Submitted To The National Aeronautics and Space Administration

    Lyndon B. Johnson Space Center in Fulfillment of the Requirements

    of Con tr.-•:: :~AS

  • , .

    D 180-22876-6

    FOREWORD

    The SPS sptem definition study was initiated in December 19'6. Part I w~s completed on Ma)· 1. I 9i7. Part II technical worli. was completed October 31, 1977.

    The study was managed by the Lyndon 8. Johnson Spa.-::e Center (JSC'I of the ,.;ational Aeronautics anJ Space AJministration t1'ASA t The Contracting Officer's Representative (COR) was Clarke Co,·ington oi JSC. JSC study mana£ement team members included:

    Dickey Arndt Microwave System Andrei Konradi Space Radiation Analysis En,·ironment

    H;srold Benson Cost Analysis Jim Kelley Microwa,·e Antenna Bob Bond Man-Machine Interface Don Kessler Collision Probability Jim Cioni Photovoltaic Systems Lou Leopold Microwa\"e GC

  • 0180-22876-6

    This report was prepared in 8 '\'Olumes as follo,.·s:

    I - Executive Summar)' II - T echnicaJ Summary Ill - SPS S.itdlitc Systems IV - M trow ave Power T nnsmission

    Systems

    iii

    V - Space O~rations VI - Euluation Data Book VU - Study Part II Final Briefing Book VIII - SPS Laun.:h Vduclc Ascent and Enlry

    Sonic °'·erpressure and Noise E ffects

  • ORIGINAL PAGE J& OF POOR QUAUTY

    01~22876-6

    TABLE OF COl\'TE!\'TS

    Titlr

    1.0 l~IRODUCTI01' ....................................................... .

    .:.o \t:\SS PROPERTIES ..................................................... . .:.1 Silicone PhotO\·oltaic Referen.:e System ............................. : .... .

    .: . I. I Summary Weight Statement ..................................... .

    .: .1.1-1.0 Solar Enern Collection S)·stem ......................... .

    .:. I.I-I.I Primary Structure ........................... .

    .:.1.1-1.: Se..:ondal') Structure ......................... .

    .:. l.l- l 3 '.\k.:hanical Rotary Joint ...................... .

    .:.1.1 ·l.4 '.\lainh:nan..:e Station ......................... .

    .:.1.1-1.5 Control ................................... .

    .:. l. l-1.6 Instrumentation ·Communications ............... .

    .: . I. i -1. ~ Solar Cell Blankets .......................... .

    .: .1.1- l.8 Solar C oncentr.nors .......................... .

    .:.1.1-1.Q Power Distribution .......................... .

    I

    3 3 5

    5 .. I ....

    30

    31

    3.: 43

    44

    : l.1-.: .0 \fo:rowaw Power T r:msmission System. . . . . . . . . . . . . . . . . . . . . 51

    .::.1.:.:.0 Weight Growth Allowance............................... ttO Rankine Th;:rm;.I Engine Refrren..:e S~·stem . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 115

    3.0 COST DATA P.-KKAGE ................................................... 143

    3.1 Introduction ........................................................ 143

    3 . .: Cost Estimating Details ................................................ 145

    3.3 Reference Thermal Engme-Co~i Data Package .............................. .:o.: 3 .4 '.\onrecurring Cost .................................................... .:.:s

    4.0 U~CERT AIST"\. ~\~ . .\l )'SIS D:\T . .\ P . .\(K.o\GE ....... , .............. _ ....... _. "'"7

    4.l ...\ppr,1.1..:h and Summary ............................................... .:..:7

    4 . .: Component and Element Uncertainties .................................... .:..:9 4.3 Size Mass Uncertainty ................................................. 240

    4.3.1 Photovoltaic Size/Mass Uncertainty ................................ .:40

    4.3 . .: Thermal Engine Size 'Mass Uncertainty .............................. 185

    4.4 Mass/Cost Uncertainty Sotes ........................................... .:88

  • APPE1'1>1X A APPENDIX B APPENDIXC

    APPENDIXD APPENDIX E APPENDIX F

    APPESDIXG

    APPESOIXH APPENDIX I

    ENCLOSURE l

    Dla.22876-6

    APPENDICES

    Siling Data for a :o Meter Long Tapered Tube of GraphiteiEpoxy . . . . . . 6: Amy Edae Loading Analysis . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10

    loads Analysis and Loads/Sizing Summary for Critical Beam in Vpper Surface. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 74

    Weight Analysis of :OM and SM Beams. . . . . . . . . . . . . . . . . . . . . . . . . . . . 84 Weight Analysis of 70 KW Klystron . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . JO I

    Scaling Rr:lationships for Column Load on Critical Strut

    in Criti~l Beam ................................... .

    Structural Planform Sizing. Reference Lr:ngths of :o Merer Beams. and Design loads. Strut Sizmg. and :o )lcter Beam Umr Wr:ighrs

    11:

    for Nominal.. &st and Worst Configurations . ....... * •••••••••••••• ~57 \'ariation of Structure \\'eight with Structural Planform Area ........... ::o Crippling Coefficient Uncertainty for SPS Graphite/Epoxy Tubes . . . . . . . :s 1

    ENCLOSURES

    \lani.lfacturing Analysis-Tr:~tri;il Fabrication oi Primary

    Structure Strut Assemblies .................................... Ibo

    llRh;('\AL P:\HF. lb 4\F PWH. 1.tLALll'Y

  • Dl80-2287U

    SPS SYSTEMS DEFINmON STUDY

    Part II final Report

    Volume6

    Evaluation Data Book

    1.0 INTRODUCTION

    This volume bas been prepared to rrovide a permanent record of the actual calculations of mass

    properties, costs. and uncertainties for the Part II final reference designs. The data are presented

    ·with only the .necessary amount of exploratory text. The analysts' original notes have been used

    whenever adequately legible in order to preserve authenticity.

  • Dl80-2287U

    2.0 MASS PROPER.TIES

    2.1 SILICON PHOTOVOLTAIC REFERENCE SYSTEM

    This weight definition and uncertainty notebook for the photovoltaic reference configuration is a

    supplement to the fonnal documentation provided in support of the Part 11 final review.

    The weight definition part of this notebook provides weight data to a lower level of detail than was

    presented at the final review. Included in the weight defi11ition are semi-detailed weight summaries.

    weight calculations. drawings and sketches. and resu:ts of weight analysis studies. A preliminary

    loads and stress analysis for the critical beams in the basic structural frame is also provided.

    The weight uncertainty part of this notebook provides the base data pertinent to the establishment

    of the satellite weight/size tolerance ellipses. Subjects addressed are I) the variatior of saiellite

    weight with array planfonn area. and ~ l the effect of tolerances on the weight of the reference

    configuration.

    Analyst: Bob ("on rad

    f.b:E.'CEDING PAGE J3LANK NO'l' FILMED

    3

  • Photovoltaic Reference ~onfigurati~n ~· - lllllNO----

    SPS.1004

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    Fl 660 am ~

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    :zs:zsz~ [

    47/Jm ZSZSZSZS.,_ . · zszszszs_ .. ...___-:............rti~ni zs ZSZS..=;>.. · __ It __ 24080m r-

    TOT AL SOLAR CELL AREA: 97.34 Km2 TOTAL ARRAY AREA: 102.51 Km2 TOTAL SATELLITE AREA: 112.78 Km2 OUTPUT: 16.43 GW MINIMUM. TO SLIP RINGS

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  • Photovoltaic Reference Panel to Array Assembly ______________________ .._ ____________________________________________________ .114'11.Nll ____ __

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  • Photovoltaic Reference Solar Array Arrangement and Attachment

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  • DllO-Ul'76-6

    l.O COST DATA PACKAGE

    J.l INTRODUCTION

    ne final Part II cost estimates utilized the Boeing parametric cost model and the mature industry costing methodofosies developed durin1 the study. The procedure used was as follows:

    Tbe rust step was to make cost estimates for DDT&E and rust unit costs using the parametric cost model.

    The parametric cost model predicts costs for typical aerospace products at typical aerospace pro-duction rates on the order of 100 units per year or less. Many of the items in these SPS•s must be produced at ttlatiYely hi&h production rates to mttl any reasonable SPS deployment scenario. Hardware produced at high rates employs different tooling concepts and different production

    awthods. more similar to mass production than typical aerospace tt\.-hniques. Correlations deYea. oped for a wide variety of p:oducrs indicate a production rate. cost improvement slope of approxi·

    nzarely 70%. Adjustments fo the PCM results for hish pl'Qduction items were made as follows: First. a standard hours estimate of typical aerospl\.--e costs was developed utilizing a typical ilero-

    spacc cost impnwement slope for I .000 units.

    (Experience of jetliner production indicates that approximately l ,000 units production arc required

    to reach the standard hours .. predictable by tasks/timeline/headcount analyses.) A production rate

    improvement factor is then calculated based on the ratio of required annual production rate to a

    typical aerospace product value of 100 units per year. A production rate improvement slope of

    70% was used.

    In certain instances detailed estimates were available for manufacturing costs. These were used as available.

    Total SPS system costs include also costs for space transportation. costs for space construction

    operations, and costs for ground receiving stations. Details of the launch vehicle cost per flight esti·

    matins procedure were reported in Volume V of the Part I Final Repon. launch vehide ;,;ost per

    flight is dependent on launch rate.

    Total transponation costs included transportation of propellants and orbit transfer hardware to low

    Earth orbit. and in addition the cost of orbit transfer hardware feither .11emical orbit transfer vehi· cles or self-power electric orbit transfer system installations depending on construction location).

    Construction costs im:luded the transportation 'osts for crew rotation and resupply. the crew opera·

    tions support costs and rhe amortization of construction base c. · .s using typkal capital facilities

    amortization procedures. Construction base habitats and basic structure were amortized over a ~5

    143

  • Dll0-2217"6

    year period with the construction equipment amonittd over an 8 year period. Crew transportation

    C.:'lSts presumed for the I SPS per year rate. the use of a modified shuttle v:hicle at SI~ million rer

    flight and for the 4 SPS per year rate. the use0

    of an advanced fully reuseable shuttle at SS million

    per flight. Delivery ofpropeUants to low Earth orbit for the crew rotation and resupply orbit trans-

    fer \'Chicles is assumed to occur with the laeav)' lift launch vehicle at the appropriate cost per flight

    figure. ~C~ts for orbit transfer installations for the self-power case. were derived usin1 the paramet-

    ~ cit model with production rate adjustments for hith production items as previously discussed.

    144

  • 3.2 COST ESTIMATING DETAllS

    Table I in the cost data pad:aatris a capital cost summary for the photovoltaic SPS. It summarizes total costs in itecordance with tk wort bre3kdown structure teMrally used a11d indicates source

    data and references f\lfther backup tables that provide additional detail. Interest during COt\Stru.:-tion is added to the total costs based on an cstunateJ construction period. Growth is added to pro-

    vide a cost equiv;Uent of the mass growth projectfuns developed and the mass uncertainty analyses.

    Tabk 1 summarizes the mature industry tstim6lte. Table : aocs to a le>1el of work b~akdown struc· ture t-tlow that of Table l. tl\ote that the .. other .. cate¥Cn from the first part ofTahh:: is

    included in the multiple

  • sra.:i: i;onstrui:tion crew rcprc~nts two "'rewi. to a.:count for time off duty (90 days in sp.tce and 90

    days ofn. with a IO'; margin, and provides a crew surrorr staff of tl>'n peorle for each crew man working in space. Tabk 13 summarilt>S transportation costs estim;Ued. Table 1.i provides the

    mature industry 1.-ost estim:ate for the self-powered orbit transti:r system. In this case the system

    nlStl'd indud~ mass p:owth and the mass 1rowtb was ddeted and the ,·alues earned in Tablt' 13. Tal\k IS is the paranwtrk cost model run that provides the raw data from whi.:h Toable 14 was prl'·

    ran:J. T abli: 16 summarizes crew rotation and resupply n-qui~ments. Table I 7 summarizes the

    cakulations of cost growth ~uivalent to the maS') growth detennined fron1 the uncertainty anal-}·ses. Table 18 sununariz~ LEO versus GEO cost differtnct!'s. Tables 19 thru ~7 pfO\·ide a similar

    1..·ost radtat?C for th~· tht>nnal engine system.

    146

  • TABLE 1 CAPITAL COST S1.114ARY - PHOTOVOLTAIC SPS (SILICON CR-1)

    WBS I ITEM SOURCES & REFERENCES 1 SPSlYR 4 SPSlYR LEO CON· GEO CON- LEO CON- GEO CON-

    STRUCTION STRUCTION STRUCTJON STRVCTION . 1.01 Solar Power Satellite (7442) (7190) (5587) (5378)

    1.01.00 Multiple/Connon . Mature Industry Estimate, Table 2 897 793 760 661 • Mature Industry Discussion • Parametric Cost Model Run, Table 3

    1.01.01 Energy Collection . Solar Cell Costs, Table 4 0 0 0 0 1.01.02 Energy Conversion • Solar Cell Cost Discussion, Volu111e II 3731 3588 2793 2686 l.01.03 Power Distribution • Structural Mfg Estimate. Encl. 1 138 133 82 79

    • Varian Analysis of Klystron Production 1.01.04 Microwave Power • MPTS Error Analysis 2676 2576 1952 1952

    Transmission . SPS Mass Estimate, Table 5 & Backup " LEO Figures Reflect SS Oversize -- .. ·-- - -··· --- -·-------

    ~ 1.02 Ground Receiving Station . Rectenna Cost Estimate, Table 6 (4446) (4446) (4000) (4000) I . Bovay Studies (JSC Contract ) • Raytheon Studies (Various Contracts) . Rectenna Optimal Sizing Analysis

    --------·---·------- ------- ------· 2.0 Construction/ (1109) (1126) (1109) (1126)

    Space Support

    2.01 Construction B~se Writedown Sunnary, Table 7 596 620 596 620 (Facility Wrltedown) . Facility Mass & Cost Estimates,

    Tables 8 & 9 Construction Analyses & Base Definitions (See Volume V)

    2.02 Space Support

    2.02.01 Staging Base . Stagi n~r Base Hass & Cost Estimates, Tables 10 & 11 N/A NIA

    2.02.02 Crew Support Crew Support ROM Estimate. Table 12 497 506 597 506 • Crew Reqts from Construction Analysis

    (Parts I & II Doc1M11entation)

    2.02.03 Other OPS Support 16 16

  • TAOLE 1 CAPITAL COST SIJot4ARY - PHOTOVOLTAIC SPS (StLICON CR•l) (CONT)

    WBS II ITEM SOURCES & REFERENCES 1 SPs,~g 4 SPS[YR l. £0 CON- . -COH- [EO coN- GEO CON-STRUCTION S!RUCTI.QN STRUCTION s·.·~ucTION

    3.00 Space Transportation (6445) (9780) (4188) . ~652Z)

    3.01 Earth - LEO Numbers of Flights & Costs Sunwnary. Table 13

    3.01.01 freight . Cost Per Flight Analyses (Parts I & II Ooci.nenta t ion)

    3139 2415 2155 165R

    3.01. 02 Crew Cost Per Flight Discussion, Volume II 336 336 140 140 3.02 LEO-GEO HLLV Operations Studies, Contract NAS 3.02.01 Freight . OTV Performance (Volume V} 2816 6670 1790 4482

    . OTS Performance (Part I) 154 359 103 242 = • OTS Mature Industry Estimate, Table 14 -• . OTS PCM Run, Table 15 ' CID N FSTSA Reports (Contract NAS9-14323) f • Crew Rotation & Resupply Sumnary, Table 16

    • Crew Duty Cycle Studies (Part I) • Advanced Earth Orbit Transportatton

    Systems Technology Requirements (Contract NASl-13944)

    -·--·---·· Interest During Contruction/Transportation Timel i nes (700 days) (450 days)iS66 days) f 3G6 days) Construction (1864) (1388) 1154) 851)

    - . -· ··-·-------------- . Growth . Table 17

    Uncertainty Analyse; (3450) (4034) (138) (1094) • FSTSA M.-~ss/Cost Growth Correlation

    Total 24,756 27,964 _1_~!!!!_ __ 18.971_ -------- ----·-- -- ., - ·- -···-· ·- . - ---·- -- . --·- . --... -- ---~--·--·-·· --~ .. -·-----·

  • TA!:.E 2 MATURE INDUSTRY ESTIMATE, PHOTOVOLTAIC SPS AND MPTS

    PCM FULLY MATURE MATURE UNIT LEARNED INDUSTRY INDUSTRY

    ITEM & MASS {LB} NJMBER SLQfL CQ~T PCM TFU Y.f!ll.._ !QI&. •l SPIL!R M 2SlY8 !&LARl!S§ P/V SPS !1 7~5 1712 314tS120Q OTHER Hl1lll 1661971 . HULT/COM l3Z1178 564 126t PRIM STRUC 1,824 .85 2,375 971,550 470 857,615 •• H01990 •• 1t0.a!190 50 (fr• 72501 Mfr, Est) !!L~Q~! .. lH:al!! 79 879 ----·-'··-THRUSTERS 110 Lb. 640 .85 1,328 243, lSO 262 168,260 66,510 33,255 2,082 PROCESSORS 12.000 Lb. 12 .85 6,248 51,550 1,236 14,843 42,848 21,424 655 STRUCTURE 10,000 Lb. 4 .85 7,505 25.140 1,485 5,943 H,140 14,860 1,637 a -TANl(S 1.130 Lb. 8 .85 1.040 6, 178 206 1,647 5,823 2,912 1.420

    i - INSTRUM. 1,000 Lb. 4 .85 3,752 12,570 742 2,971 12,570 7,428 8,188 ~ tttfI86L.,(1jeUit.~OO.Lb 3 1.0 7,385 28,157 9,385 28 157 ..• H:al!Z 28 157 ......... _____ , ___ 'Qttj!J~l,.iaOOO.Lb· 3 1.0 24,576 73,729 24,576 73 729 •• .Z~aU! ... n,nt ___ ,, ___ &Ht.iO,E.lJaSOO.Lb. 2 .85 12,145 22.501 .M.H:a!el 22 501 ---··'···

  • TABLE 2 (Continued)

    PCM FULLY MATURE MATURE UNIT LEARNED INDUSTRY INDUSTRY

    ITD1 & MASS ILB} NUMBER ~ CQST PCM TFU UNIT TQTAb_ '1 iPllY8 t4 IPIL " ...... DObLARLl

    Jtt, 221. SOLAR BLANKETS .8 15,056 9,945,16S

    ARRAY PANELS 1 Lb. 78,387,000 .8 17 3,365 2,633 3,588,000 2 , 563 , OCl'I $3S/M2 I $25/M2

    JUMPERS 0.01 Lb. 78,387,000 .85 0.123 .024 2,537,800 16,000 16,000 $45/KG

    NETWORK 6,l24 .85 444 87 538,300 68,786 68,786 $25/KG

    CATERNARIES 6, 124 .85 496 98 601,341 76,842 38,421 $30/KG ~ -- POWER DISTRIBUTION 132.856 78,956 i ~ SWITCHGEAR 1,320 Lb. 208 .as 3,787 292,000 750 156,000 108,000 54, 100 868

    BUSSES 15,000 Lbs. 32 .as 626 11,276 124 3,966 7,000 7,000 $32 ROTARY JOINT 38,000 Lb. 2 .85 9,639 17 ,8S6 17,856 17,856 $560

  • TABLE 2 (Contfnued)

    PCM f'ULLY MATURE MATURE UNIT LEARNED INOUSTRY INDUSTRY

    ITEM & MASS (LB) ffUMIER .&m. &.m. M UNIT _ I2tAI.. N IHJ8 14 ¥HJ" DOU.Ml !CJi ) MPTS TOTAL (2 Ant) ~.1Zl11JI l1Hl a!H CHECKOUT I PKG'G l!1RR9 HaOOO tllLT/CCJ4 311.0jj !llalZI in.uz PRIMARY STRUC 240 .85 431 21,760 (965 Lb.)

    85 20,478 u.211 6,609 125

    SEC STRUC (7,137 Lb) 122 .85 2,344 69,857 464 &6,613 51,25' 25,627 129

    ATT CONTROL (1.000 Lb) 24 90 13,278 124,529 4,646 111,515 201,736 111,511 21,000 •

    - CENTRAL CCJ4PUTE 6 l 9,385 28, 157 9,385 56,310 56,310 56,310 41,000 I "' - (500 Lb) CC»llJNIC (2,000 Lb) 6 1 24,576 73,129 24,576 147,456 147,45' 147,456 27,000 f POWER OISTRl8UIION 1. 188.a.061 •H1!17 - !4§.IQZ PWR PROC (12,000 Lb) 456 90 3,497 410,414 i,223 558,000 261,317 261,317 105

    SWITCHGEAR (660 Lb) 912 85 2.120 299, 137 420 382,767 126,746 63,373 464

    THERMAL CONTROL 456 85 3,476 287,699 (3,600 Lb.)

    688 313,800 '"'·"' 7J,474 197

    :1 ~>

    A:; t""'

    ~ ;; t i:: ~~ ' El

  • ITEM & HASS (LB)

    POWER DISTRIBUTION (7,000 Lbs.)

    ~BARRAYS

    STRU:TURE AND Wf.'!EoUIDES (685 Lb.)

    KLYSTRONS ~ (70 KWRF)

    THERMAL CONTROL

    CONTROL CKTS (11 Lb.)

    TABLE 2 (Continued)

    PCM UNIT

    FULLY LEARNED

    NUMBER SLOPE COST PCM T£Y. UN IT TQJ Al

    456

    13,864

    194, 112

    194, 112

    194, 112

    85 2,306 190,818

    85

    90

    85

    90

    323

    6,707,654

    368,651

    53 687,240

    157 1,762,474

    300 3,889,287

    457 208,175

    64

    18 3,600,136

    31 6,033,318

    105 20,378,131

    MATURE INDUSTRY '1 SPS/YR

    97,486

    MATURE INDUSTRY ,4 2}/YR

    48,743

    11519,069 !1103,399

    258,439

    524, 102

    274,000

    462,528

    258,439

    339,696

    274,000

    231,264

    60

  • NO

    I TOTAL ,.OIU" 0

    I PIDll INTIG I NGMT 0

    S PNOTOV "' 0

    4 PL T SYS HD 0

    VI w

    5 :.llSTAINING 0

    651 ' I 0

    Table ·3A P1r1111tr1c Cost Model Ou~put for Photovol t11c SPS

    IUI ILIMINT NITHOD IOUI• ILIND IU'T OTI MOD NOD NUNlll LIN TO CH PACTOll PION SI I CN"X I

    0 DDTll IUll 0 O.H • • • ••• O"ODI• 0 UNIT SUH 0 o.oo 0 • • OPCODI• •

    1 DDT II UCTOI I .... • • 0 ••• OPCDDI• I UNIT UCTOI I O.H 0 • I OPCODI• 2

    ' DDTll IUll 0 o.oo 0 • ·• ••• OPCODI• • UNIT f,UDI 0 o.oo 0 0 0 OPCODI• I

    J DDTll IUH 0 o.oo • • • ••• OPCODI• 0 UNIT SUH 0 o.oo • • • Of'CODl• •

    J DDTll PAC UN 4 o.os 0 0 0 o.o DPCOOI• J

    UNIT Nl'A 0 o.oo 0 • 0 OPCODI• I I DDUI CU• 4 o.oo 0 0 I o.o

    OPCODE• II 12 o.oo UNIT Nl'A 0 o.oo 0 0 0

    OPCODE• I

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    11.111 ....

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    "''" 0

    • -i

    if I!

  • NO NAMI

    1 FLT SYS DD&T 0

    • SYSTIK TUT 0

    ' SYS TUT Lii D

    - TIST HDNI ~JO SI 0

    11 FLT TUT HDNI 0

    u SOFTNARI INH 0

    Table 3A (continued) IUI ILIMINT MITHOD IDUR• ILEND SUPT OTI MOD MOD NUMllR LIN

    TO CU UCTOU l'ltOH " " CH'U "

    0 DDUI FACTOR It LOO 0 0 0 o.o O,COOI!• 2 ' 1.00 ' 1.00 UNIT N'A 0 o.oo 0 0 0 OPCODI• •

    J DDr&L SUH 0 o.oo 0 0 0 o.o 0'CODIE• 0

    UNIT IUA 0 o.oo 0 0 0 OPCODE• •

    • DDTH CU• " o.oo 0 0 0 o.o O,CODI• U Jlt o.oo UNIT tlJIA D o.oo • 0 0 O,CODI• I

    • DOTH FAC UN " o.oa 0 0 0 o.o orc:on1• J UNIT NJIA 0 .... 0 • 0 0'CODI• •

    • DDTll FAC UN " o.oa D 0 0 o.o DPCODI• J UNIT NJ'A 0 o.oo • • • OltCODI• •

    • DDTU CU• 7 o.oo 0 D 0 o.o OPCODE• II ST o.oo UNIT "'" 0 o.oo • 0 0 OP'COOI• •

    COIT fODOJ

    0

    •

    71',tU

    0

    ........ •

    111107

    •

    111.01

    •

    no.•71 0

    ..

    ~ -i

  • Table 3A (continued) NO HAif i SUI ILININT NfYHOD SOUi• ILIND SUll'T OTS "OD "OD HUNlll LIN

    TO en FACTOll FIO" • • Cf"ll'LX ..

    u CSI , DOTH FACTOI "'

    o.u • 0 • ••• 0 Oll'CODI• l UNIT FACT DI " o. u 0 I 100 orcooi:• '

    ... TOOLING J DDT&I FACTOI "' o.u 0 • 0 0.1 0 Ol'CODE• I UNIT Nl'A 0 o.oo • 0 0 Ol'COCIE• a

    IS ASSY & C.fO J DDT&I N.fA 0 o.oo • 0 0 o.o 0 OPCODI• • UNrT FAC UN " 0.07 0 • • Ol'CODE• J u "U&.T.-CON " DOT&I SUH 0 o.oo 0 0 0 o.o - 0 Dll'CODI• 0 "" UNIT SUH 0 o.oo 0 • • "" Ol'COOE• 0 17 l'llN STIUCT u DDT&I CU LOO JO 0 D o.o

    7250 LIS Ol'COOE • UNIT cu "'' 1.00 0 1114 14 O,COOE• l

    AOOllGATID VALUll

    11 ATT CONTIOL u DOTH SUH D o.oo • • 0 o.o 0 Ol'COOE• 0 UNIT SUH 0 I.DI 0 • 0 Ol'CODI• 0

    COST COOO)

    .. , .... llolt,Hl

    uo.uo

    •

    • 1"'61141

    .... "' .... ., .. ,,. 6,Hlt

    ,, '" ,,, ,.,..

    ua.-.u ua.Ht

    ~ -! f

    ~@ g?) ..... z

    ~ ~; ['-f

    €.,,

    &!

  • NO

    If THIUSTUS 110 LBS

    20 PROCUSOPS 11000 LH

    21 STRUCTURE 10000 us

    -"" °' u TANKS 1130 LIS

    n INSTIU" 1000 LIS

    Iii CEHTUL CO"PUTI 500 LH

    Table lA (continued) SUI &LEKINT HfTHOD sou•- ILIHD IUPT OTI KOO HOD NUHl!I LIN

    TO cu '4CTOllS uo" " " c""·· "

    18 Dl>T&I CU u I .OD JI 0 0 o.o. OPCODE•

    UNIT cu " 1.00 45 '"° Ill OPCODE• AIPllGATID VALUll

    II DDTU CU ,.. a.oo JI 0 I 1.0 O"CODE•

    UNIT CER u o.to 0 u '" OPCO:>t• AGGllOATID VALUIS

    JS DDT&E CU z 1.00 JO 0 0 1.0 OPCODE•

    llNJT C£11 u 1.00 0 " '" nPCODE• 1 AOOIHATID VAL UH

    11 DDUI CU I a .OD JO 0 0 1.0 OPCODE•

    UNIT cu "7 S.00 "' • "' OPCODE• AIOllOATID VALUll

    •• DOTH CU ., 1.00 SI Cl 0 o. Cl OPCODE• UNIT cu '° 1.00 "' " 1111 OPCODE• 1

    AOGIHATID VALUIS

    u DDT&I CU If l.00 Sl 0 to s.o OPCODE•

    UHJT cu "' S.00 0 s 110 OPCODI• AOGllGATID VALUll

    COIJ HOO>

    1.u1

    1,u1

    us. no

    u.tu •• 11111

    tl1HI

    so,u, 715DS

    u,1tiio

    ", ,, 7

    1.00

    ,, 171

    u,,,, 11751

    u.no

    o.sn f,Jlf

    11.111

    c:. -i

  • NO NAMI

    ZS COMltUNIC zooo LH

    26 f'WI GIN 0

    27 SOLAI ILANICITI 0

    -"' ...... 21


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