Embed Size (px)
Citation preview
ii!_
NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNASA CP,-
./3
(NASA-CR-134426) WIND IUNNEL TESTS OF AN N75-1_81_O.015-SCALE CONFIGUSATIOB 140A/B SPACE
SHUTTLE ORBI_EI MODEL (b7-G) IN IHE NASA/LRC
8-F6CT T_T TO OBTAIN TRANSONIC AE_OEYNA8IC Unclas
F05C£ DATA (OAIOb) (Chrysler Corp.} 197 p G3/18 Ob666
SPACE SHUTTLE
AEROTHERMODYNAMIC DATA REPORT ,,"F _
, _,. . _
¥
"&,
JOHNSON SPACE CENTER g_YN N_Jag_ment services ;_1
s,,,¢, o,v,s,o,,@ CHRYSLERHOUSTON, TEXAS CO.POn_TOON
, , ,, , , n mn Ill IIII II IIIII I Illll I I n_.....
197500674.7
https://ntrs.nasa.gov/search.jsp?R=19750006742 2018-08-01T17:03:48+00:00Z
October, 1974
DMS-DR-2120NASACR-134,426
WINDTUNNELTESTSOF AN O.OI5-SCALE
CONFIGURATION140A/BSPACESHUTTLEORBITER
MODEL (67-0)INTHE NASA/LRC8-FOOTTPT
TO OBTAINTRANSONICAERODYNAMICFORCEDATA
(OAl06)
by
R. BurrowsRockwellInternationalSpaceDivision
PreparedunderNASA ContractNumberNASg-13247
by
DataManagementServicesChryslerCorporationSpace Division
New Orleans,La. 70189
for
EngineeringAnalysisDivision
JohnsonSpaceCenterNationalAeronauticsand SpaceAdministration
Houston,Texas
1975006742-002
P
WINDTUNNELTEST SPECIFICS:
Test Number: LaRC 8-Foot TPT 668NASA Series Number: OAI06Test Date: 17 through 18 December 1973Model Number: 67-0Occupancy Hours : 24
FACILITY COORDINATOR:
David StoneLangley Research CenterSSD, Vehicle Analysis BranchBldg. 1247-B, Room 120BMail Stop 163-ALangley StationHampton, Virginia 23665
Phone" (703) 827-2483AERODYNAMICSANALYSIS
PROJECTENGINEERS" ENGINEER:
R. Burrows Bernard Spencer, Jr. Tom CorneliusMail Code AC()7 Langley Research Center Mail Code AC07Rockwell Int'l Space Div. SSD, Aerodynamics Sec. Rockwell International12214 Lakewood Blvd. Bldg. 1251, Room221 12214 Lakewood Blvd.Downey, Calif. 90421 Mail Stop 411 Downey, Calif. 90421
Langley StationPhone: (213) 922-2440 Hampton, Virginia 23665 Phone: (213) 922-1526
Phone: (703) 827-3911
DATA MANAGEMENTSERVICES:
Prepared by: Liaison -- V. W. Sparks, D. A. SarverOperations -- Maurice Moser, Jr.
Reviewed by: G.G. McDonald, J. L. Glynn_) _"
Approved : _ . ),_ _ , _ _____ Concurrence: !____ ,'_L.Kemp, Mnm_n-_age-r j.F/'G. Swider, ManagerData N_anagementServices Flight Technology Branch
Chrysler Corporation Space Division assumes no responsibility for thedata presented other than display characteristics.
ii !' l
i 975006742-003
.................._......_ ............1 F............. ! _ _ ....... .i i : iI
I , i ! t
liWINDTUNNELTESTS OF AN O.OIS-SCALE CONFIGURATION140A/B
SPACESHUTTLEORBITER MODEL(67-0)
IN THE NASA/LRC 8-FOOT TPT TO OBTAIN
TRANSONICAERODYNAMICFORC[ DATA (OAf06)
By R. Burrows, Rockwell InternationalSpace Division
ABSTRACT
This report contains the results of wind tunnel tests of the NASA/
Rockwell O.Ol5-scale Configuration 4 (140A/B) Orbiter model (67-0).
These tests were conducted to obtain longitudinal stability and
control data for Mach numbers from 0.35 to 1.2. Data were obtained for
an alpha range of -2 ° to +22° at beta = 0°,
The effect of speedbrake deflection and body flap deflection was
obtained through the Mach range. Boundary layer transition strips were
used on the model.
iii
;j
1975006742-004
i iI i
'! _ I I
" TABLE OF CONTENTS
Page
ABSTRACT iii
INDEX OF NOD(L FIGURES 2
INDEX OF DATA FIGURES 3
NOMENCLATIJRE 4
CONFIGURATION INVESTIGATED 7
TEST FACILITY DESCRIPTION 8
DATA REDUCTION 9
TABLES
I. TEST CONDITIONS lO
II. DATA SET/RUN NUMBER COLLATION SUMMARY II
Ill. MODEL DIMENSIONAL DATA 12
FIGURES
MODEL 21
DATA 25
APPENDIX
TABULATED SOURCE DATA
.... 11................................. i|i i i i I]
1975006742-005
INDEX OF MODEL FIGURES " "
Figure Title Page
I. .Axissystems. 21
2. Model sketches.
a. Orbiter three view showing component nomenclature 22
b. SSV orbiter configuration 140A/B general dimensions 23
c. Boundary layer transition strip locations 24
C_
] 975006742-006
¢,,."0 aJ •
•r- _ _
,--. q,.. e," va. aJu
o_¢_3
.i
......... I I lli Ii ................. :1 _ J - _ " " _ 4
1975006742-007
NO_ENCI_u_RE
General
SADSAC
SYMBOL SYMBOL DEFINITION
speed of sound; m/see, ft/sec
Cp CP prezsure coefficient; (Pl - P_)/q
M MACH Mach number; V/a
p pressure; N/m 2, psf
q Q(PSF) tunnel free stream dynamic pressure, psf
RN/L RN/L unit Reynolds number; per m, per ft
V velocity; m/see, ft/sec
(_ ALPHA nLgle of r_ttsck, degrees
BETA :n,g]e off sideslip, degrees
P',.',[ n*f;]_ Ol yuw, degrees
# PHI mlgle of roll, degrees
p m_ss density; kg/m 3, slugs/ft 3
Reference & C.G. Definitions
Ab bnse nres; m2, ft2
b BEEF orbiter wing span; lateral reference length
c.g. cen_er of gravity
_IEF LNEF M.A.C. longitudinal reference length, in(,
i: ',.;;_._EF orbiter wing area reference area; ft 2
MRP m,mt_mt r i'(T,:r_uu point, in orbiter coordinate system
X_Id<P m_::vr_ r,l r_tlc_ point on X txi:;
YMJ",P mrm_,,l_t,r [er_;nc,_point on Y _xi:;
'/lV(}d) r_l_,m,,r_tr,,t',,r,,rl,.'r_ point on Z ',zic
:',l; k;(:iGY'l'::
i l,,,",l;t ti <or_dltion:;
t tot_l cotldltionIr " ::trr Jm
4
197500674P-002
NOMENCLATURE (Continued)
Bg,_y-AxisSystem
SADSAC[
i _ _ DE,raiSON
ON C_ normal-force coefficient; normal forceqS
CA CA axial-force coefficient; axial forceqS
Oy CY side-force coefficient; side forceqS
CAb CAB base-force coefficient; base forceqS
-Ab(Pb- p®)/qs
CAf CAF forebody axial force coefficient, CA - CAb
Cm C_ pitching-moment coefficient; Bitching momentqSIR
Cn C_N yawing-moment coefficient; _awin 6 momentqSb
C_ CBL rolllng-moment coefficient; rollin 6 momentqSb
Stability-Axis System
cL CL lift coefficient; llf___ttqS
CD CD drag coefficient; dr_gqS
CDb CDB b_se-drag coefficient; beSeqsdra_
CDf CDF for,:_ iy dr_g coefficient; CD - CDb
Cy CY side-force coefficient; side forceqS
Cm CLM pitching-moment coefficient; _itching momentqs&
Cn CLN yawing-moment coefficient; _swin_ momentqSb
C_ CSL rolling-moment coefficient; rollin_qsbmoment
L/D L/D lift-to-drag ratio; C_C D
5
L.-. ............ - .......................... _ ----_ " "
1975006742-009
r
NOMENCLATURE (Continued)Additions to b_andard List
SADSAC
S_.ymboI Sm_l__ L)efinition
_B orbiter body length
Xo orbiter longitudina'istation, in
Yo orbiter spanwise station, in
Zo orbiter waterline, in
,,sa AILRON aileron deflection (6eL - _,eR)/2,degrees
'_e ELEVON eIevon deflection (_eL + ,seR)/2.degrees
'_r RUDDER rudder deflection, degrees
,_ BDFLAP body flap deflection, degreesI;F
'_SB SPDBRK speedbrake deflection, degrees
A,sSB DSPBRK incrementalspeedbrake deflection, degrees
XCp/_B XCP/L center of pressure location based on body length,
XC.G. CL_M _ref
_-B-_- CN _B
XCp XCP/L ALPHA=IO center of pressure location based on body length_B _:lO
,itan angle of attack of ten (lO) de_]rees
CDmi, CDHIN J,ini,lu,_(Jrdycoefficient
I)CLM/DSPI)RKpitching moment coefficient derivative withAG"/ A,,.SB
respect to speedbrake deflection
CPI orbiter cavity pressure coefficient
CP2 orbiter centerline base pressure coefficient
CP3 OMS base pressure coefficient
CP4,5,6 clogged or blanked pressure taps, zero valuesare listed in source data.
6
1975006742-010
_ CONFIGURATION INVESTIGATED
The model (67-0) was an O.015-scale representationef the Space
Shuttle Vehicle Orbiter Configuration 140A/B. This configurationwas
designated as 0I, which consisted of the following components:
@26 body (fuselage)
Cg canopy
E26 elevon
F7 bodyflap
M7 OMS pod
N72 OMS nozzle
R5 rudder
V8 vertical stabilizer
WII6 wing
Mod_1 variables consisted of speedbrake deflections of O_'and 25°
and bodyflap deflections of -11.7", 0" and 16.3". Numbers I00 and 120
grit were used on the vehicle. Ir,Jnsitionstril_locations are shown in
Figure _'c.
Model component details are in Table Ill.
1975006742-011
L
TEST FACILITY DESCRIPTION
rIASA/LangleyResearch Center 8-Foot Transonic Pressure Tunnel is
an air-medium facility capable of attaining continuously variable _,lacn
numbers from 0.20 to ].30. It is a single-return,closed-circuit tunnel
having controlled stagnation tc_llperature,total pressure, and dew-point
tB_perature. The test section is 7.1 feet square. Reynolds numbers are
variable from 0.30 x IO6/foot to 7.00 x 106/foot, depending on '4_ch
nu_ber and tunnel total-pressurelimitations. Models are supported in
the test section by a sting-sectorsystBn, but wall-mounting is possible.
Schlieren photography is available for flow and shock-wave stJdies.
8 I
1975006742-012
DATAPZDUCTION
Standard LaRC data reduction methods and the following constants
were used to compute body and stability axis coefficients:
S/mbol Full Scale Model Scale
SREF 2690.0 ft 2 0,C053 ft 2
_REF 474.31 in 7.122 in
bREF 936.68 in 14.050 in.
MRP Xo I076./ in 16.151 in
Yo 0,0 in 0.0 in
Zo 375.0 in 5.625 ir_
9
1975006742-013
i i i
, I 1
TABLE I
.. , I I .TEST ; LRC 8'TPT-686 ,vAl06, DATE _ 17 DEC 73m_
TEST CONDITIONS
REYNOLDSNUMBER DYNAMICPRESSURE STAGNATIONTEMPERATUREMACHNUMBER
(perunitlenith) (PSF) (d_ees Fahrenheit)i,i
1 20 4.22 x 106/ft 881 120
0.98 4.10 x 106/ft 770 120
0.95 ;.06x10/ft #49 1200.90 3.98 x 106/ft 710 120
0.85 3.89 x lO_/ft 669 120
0.80 3.78 x 106/ft 623 120| i
0.70 3.51 x 106/ft 523 120
0.60 3.17 x '106/ft 418 120u
0.35 2.05 X 106/ft 167 120_, ., ,,
nl
i ii u
i i i i
BALANCEUTILIZED: LRC #840
COEFFICIENTCAPACITY: ACCURACY: TOLERANCE:
NF 800 Ib ± 0.5%
SF 250 Ib _+0.5%
AF 125 Ib +.0.5%
PM 1600 in-]b ± 0.5%
RM 500 in-lb _ 0.5%
YM 500 in-lb _+0.5% i
CCMMENTS:
L I I
lO
i rmlll i nll .......
............. 1975006742-014
!
1975006742-015
TABLE Ill.- MODELDIMENSIONALDATA
V_3DELCOMPO_,ENT: BODY -(B26)
GENERAL DESCRIPTION: Orbiter Fuselage Configuration 140 A/B
NOTE: B?6 identicalto B24 exceptundersideof fuselagerefairedto
acceptW116.
Model Scale = (9,_I_"
VL?'O-O00193DRAWINGNUMBER: VL70-OOOI40A
PDIMENS_Ot(S: FULL-SCALE ,MODELS_AL.
Length (Body Fwd Sta Xo = 235) - in. 1993-_ _ 19.LO0
Max. Width (at Xo = 1520) - in. ' 262.0 3._F3
Max, Depth (atXo = 1464) - in. 250.0 3.75
FinenessRatio 0._357 n=?A3y2___
Area - ft'
Max. Cross-Sectional 540.88462 0.07670
Planform
Wetted
Base
,t
:' 12 '_
.i
1975006742-016
'i
(._ TABLE Ill.- MODEL DIMENSIONALDATA - Cont:nued.
MODEL COMPONENT :_ Canopy(C9)
GENERAL DESCRIPTION: Confi_tratlon 140 A/B Orbiter_selaF, e
Model Scale= O.O15 Model DrawingNo. SS-AOOI.47VL70-OOOILOAVL70-OOOIA3ADRAWING NUMBER ,
DIMENSIONS' FULL SCALE MODELSCALE
L_gth (Xo=&3L.6_3 to 670) 235.357 3. 530
CI: "M,ex Width(@Xo=513.127) 152._12 2,286.
Max Depth(@Xo=&85.0) 25,000 0.375
Fi.e.ess Ratio .
Area , ,, _
Max.Cross-Sectional
Planform
Wetted ,
Base
, , 13
!?
]975006742-0]7
! l I ii i J
TABLEIll. Continued.
140DELCO,_IPOrIENT: s1_'o:,' L(,E2_)
GENERALDESCRIPTIO;I:Confixur_tion 140 A/B Or.biterElevon
NOTS: VLTO--OOC200data for (1) of (2) sides. Identicalto E2S except
airfoilthickness
l.!odelSc_.le= 0.015 Model DrawingsNo. SS-AOOIL8
VL70-OOC2O0
DRAWlI:GtCUZBER: VL70-OOOIAO
DII4EI61ONS: FULL-SCALE FDDEL SCALE
Area 223 5814 o.o}o)
Span (equivalent) 368.3_ ._.5._25
Inb'dequivalentchord 119.623 l.Tg&
Outb'd equivalentchord 55.1922 0.828
RatiomovablesurfaceChord/totalsurfacechord
At Inb'd equiv,chord 0.2096 0.2096
il At Outb'd equiv,chord O._OOL O./_OO&
Sweep Back Angles,degrees
LeadingEdge 0.00 0.00
-i0.056 -10.056TailingEdge
0.00 0.00Hingeline ..
Area l,loment(Normalto hinge line) , 851.1502 0.00287_
I14 '
i_. -t................ i ..... , . .. J . .J ........ _ - _ - ,
1975006742-018
TABLE Ill.- Continued.
MODEL COMPONENT: _ody _!ai', -( F7 ) .......
GENERALDESCRIPTION: , Ccnfi_u_tion]&O A/B Orbiter Body Flap
.NCr_3: Body fX&p b_s variable center].ine deflection of +13.75 ° and
-I_.25° from null position. Hinge line located at Xo =1528.3,
Zo = 28&.3 . Model Drawing No. SS-AOOIA7.Model _c_le = O.O15
DRAWlNG NUMB£R VL70-OOglLO,:_,VI,?O-OCOIA5
DIMENSION: FULL SCALE MODEL SCALE|i
Length(Xo=1520to Xo=1613)- IN. 93.000 I.395
MoK Width - IN. 262.000 3.930
Max Dtpth C:o = 152o) - IN. 23.O00 . O.%5
FinenessRatio
Aree - _2
(iJ; M'OXCross-Se¢tlona'
Plcnform ' . _ 0.0339
Wetted
Bate 41. 84722 O.OO9&l
• d
, 15s
......................... ' ,,,,,, , III|
1975006742-019
1 |
' I :/ i
TABLE Ill. - Continued.
MODEL DIMENSIONAL DATA
MODEL COMPONENT:, OMS Po#,(MT)
GENERAL DESCRIPTION :_ Conflguration_IAO A/B O_biter,OMB-POd
Model Scale = O.O15 Model Dz'awin_No. ,,_-AOOI_7VL70-OOOILOA
DRAWING NUMBER' VL70-,OOOl_.5 ....
DIMENSIONS' FULL SCALE MODEL SCALE
Length(OMSFw_ Sta Xo=1233.0) -INL 327.000 A.905
Max Width (© Xo=iASO.O) - IN. 9L.5 1./,18
109.OOO 1.635Max Depth (@ Xo=i_,93.O) . IN.
Fineness Ratio ......
Area ,, ,
Max. Cross-Sectional ,,
Plan form ,,,
Wetted ,,,
Bose L , , ,,, ,
t
• 16
:?
L .................................................. -,ik..... -' III I .... IIII
1975006742-020
_ TABLE III. - Continued. ,+
p"
v
GENERAL DESCRIFrlON: Configuration iA0 A/B Orbiter 01%SNozzle ..........
_iLch N_ulIwas mo..unted,.,at3.00_ins.t:ad of. ]5049' _s.shown on.tbe lines control
drawin_q ' ," ' ......
MODEL SCALE = 0.015 Model Drawing No. SS-AOOI&7
DRAWINGNO. VL70-OOO1AOA
DD eSIO[S SCALE MODELSCA
_kch No.
Lerksth~ in.o
Gimb_l Point to Exit PIAno _ _ __ _
Threat to Exit PiAno =_ _
I__, Diameter_ in.
Exit _
Threat
Inlet
Area --I%2.i
Exit_ u ____
Throat
Oimb_l Point (station)--in.
X 1510.O 22.77
T + 88.0 1.32
Z , &92.0 7.38 _
Null Posit_on ~ deg.
Y&W " 12° 17' 12" 17' :
17 _
1975006742-021
!....................I......................
i ! I , i
TABLE Ill. - Continued.
MODELCOMPONENT: RUDDER - R5
GENERALDESCRIPTION: Con_i_ation l&O A/B Orbit_ Jtudden .
Model Scale = 0.015 Model DrawlnE No. SS-_O01A8
DILAWINGHUMBER: VLTO-,O(_ZX)9_VL?O-OOO:L_6A
DIMENSIONS: FULL-SCALE MODEL SCALE
Area - Ft2 106.38 0.0239 .,,
Span (equivalent)- IN. 201.0 3.015
Inb'dequivalentchord 91.585 1.37_
Outb'dequivalentchord _ 0.?62
Ratioe_vable"surfacechord/total surfacechord
At Inb'dequiv,chord ....0.400 0.4,00
At Outb'dequiv,chord O.&O0 O.4oQ.
Sweep Back Angles,degrees
LeadingEdge _.83 3_.83
TailingEdge ....26.25.
Hingeline _ 3&.83 . 34.83
A(peaMoment (Normalto hinge line)-FT3 _ 0.(30178roduct o_ J_rea_and ].I_anChord_ -
18
- li!
1975006749-n99
r ........... -_ ,,_ ...... V ........ r ................ "f T....... l .................. F ............ q ............................, .........................-"i I , t ,
TABLEIll. - Continued.
MODELCOMPONENT:VERTICAL- V 8,- i z _ : ?--- _ i _ ___ 7 :_____± _ ii i. i _ •
.. GENERALDESCRIPTION:C_nfiguration .140A[B OTbit,erLyertica_i.Tail :
*_ NM_II; Similar to V5 w_th radius on TE uDDer corner #n(_ LE lower corner
_ where vert£calme_$s SV_lace. _ :_ : ...... :
t, i, =_ ,, _ __J L_
M_x;[_el_$cale =_O,Ol5 VL70-OOO]CAO_ Model Drawing No. SS-AOOI_8
D,_W*NG NUMBER,: VL?O-OOOI/_6A ....
DIM£NSIONS: FULL-SCALE MODEL SCALE
TOTDATAArea (Theo) Ftz &13.253 0.09298
Planform - : ....
Span (Theo) In _Aspect Ratio i.675Rate of Taper O.50---"-7"-O._07
, Taper Ratio _ 0._0399SweepBack Angles,degrees
Leading Edge _ __.,oo _5._TraillngEdge _,%7 25.9_7 ,,0.25 Element Line _ __+l-l}q
a_ords:
C_, Root.(Theo) i,,IP 268.5.00. L..02'750Ttp (Theo) WP i08,_.MAC 199.._756 2._Fu$.Sta. of ,25 MAC ..2_z}w.5.__..W, P. of .25 MAC _B, L. of .25 MAC o.oo o.oo
Airfoil SectionLeading WedgeAngle Oeg ._]JZJJ_----
i TralllngWedgeAngle Deg _Leading EdgeRadius _
i t- Void Area _ o.oc2Q_B1anketed Area _._JlO__._!
19
1975006742-023
i• ' " ,., : I
TABLEIII.- Concluded. P
MODELCOXPONENT" vIING-(wl_ __ L
GENERALDESCRIPTIGN"Configuration _0 A/B O_biter 'ding
NOTE: Identical to W114 except airfoil thickness. Dihedral angle is alonR_ m
trailing e.d_eof wing.__ i i !
Mode: Scale = 0.015 Model DrawLn_ No. ,_,q-_O01'.,8
VLTO-000]40BTESTNO. DWG.NO.VLTO-,)')Oz,:'J
DI_IENSlO:IS• FULL-SCALE HODELSCALE
TOTALDATA_Area--6T-_eo.) Ft2
Planform . 269_09 0.605_Span(Thee In. 936_6816_ iL.050Aspect Ratio __ 2.2_@ .... 2.265Rateof Taper ' 3.177 1.177TaperRatioDihedral_gle, d_grees(atXo-1SO6.623,Yo=__ 3. 500IncidenceAngle,degrees105,Zo- .'82.75) _ O.SO0AerodynamicT_vlst, _egrees *.._.}J-Q_19-.-y3.000SweepBackAngles,d_grees
45.00 4S_.00LeadingEd§e , .',tli.u_6TrailingEdGe .....
0.25ElementLine 35.209 35.209 .Chords:
Rc_t(Theo)B.P.O.O. 689.2429 !0.339_Tip,{Thee)B.P, -i_7,8486: _;o(,_v_c " _1 ;.tZ_ 7-_ -Fus.Sta,of .25MAC 1_126.721W.P,of ,25MAC 291.00 4.365B,L.of ,25MAC .., IB7.3349L
EXPOSEOOATA_,_'o) Ftz I512.22o5 0.408
Span,(Theo) In.BPIO8 736.6816AspectRatio 2.058 2.0S8TaperRatio .... 0,2451 0.245L•Chords
RootBPI08 570.6230 8. 559Tlp 1.00 b _ _.06
•MAC _' 354.2376 5.3]/_
Fus. Sta.of .25MAC f164.23_ i?._61,-_W.P.of .25MAC 292.OO . 4.3n0
• B.L. of .25 PAC 239.6778(__ . .3.595 _,AirfoilSection(P_ck.._ellI,'odIIA.SA)
XXXX-64Root b = 0.425 0.113 0.113
_ m i _
• 1.00 0.12 0.12TIp _ ....
Datafor 11)of (2)SidesLeadingEdGe:Cuff_Planform/.rca Ft" _ _L_U.ov_6._LeadingEdge Intersects FusH. L. @ Sta _S.O 7.575 .Leading_d_e IntersectsWing@ Sta l_uJ__._ 15_053_
2O
1975006742-024
, 71
1975006742-025
1975006742-026
?
1975006742-027
c. Boundary layer transition strip locations
Figure 2. - Concluded.
• 24
J
1975006742-028
l
DATA FIGURES
25
........... _. . ...... J_ ,,,i . d _ _" _ I
1975006742-029
" 1975006742-030
Ii J _I"FT'TTTT-'_ ;'F-_T_'T_'T Trl I I I I I I 1 I I I I 1 I I W I w I I I t l I I I I I l 1 I t l II I I I I I _
8 _ " w.
I
1 2
.1" 0 ILl
i
o: __ i ,
_r- I m
tB _" f ., --1 _
0 _ w_ F LI
ii_ _ - _ "
° ' fI--.• , =o:=". t I --t..) ..................... (44
I!_-_-_. .... _-_J._l._k ._L J_. _ I_I_L _=I.__._L..L 1 i I I t I I I l I I I I I I I | t I i , r r i II i. _ L_I.L
• • • • • • • • • • • • • W
000<1 _ --. ,-4 v o
NO '1N3101_-I-130838_I0_-I7¥_I_0N
lnnnl I
"- ' 1975006742-031
lill Illllll/IWWWW_ ...._ _,_
wq_.hqq_- • , %,\I ; i ', _ <
0 ' ' ', i I/ 1AIJ ' . i ; _' _
6. : . : _ ill
.----------'-_._--i-,e_-/---_ ........... ---- ""_ /', V/dd
- _ , 11 Y#/'/ ', _ I I ! _.<_ ' i _ %;l i .111#'1 _ , , '. , I _ , • L,¢--
_ q l , 1i'JT--l---_. ., i I I ! 1 I . ,5 ---7 { I liar, I i i i i ' ! I I / I - _•- r i t .Iii/'1 I i I ! i I ! 1 1 =,--_
I.o ooo F _ I n_ I I ', _ i I I , I I i I . u. _-
' I--- ---r--1-----------_,, -i " I __. - _lT-7--r--_, I I _<,>_1_ r--7-t-'-_-t ....._,.....{.... -i....f--'--b-i-;1 " _>
_>{_ bt 1A..Jltt I .__.....__]LI 1___1/!I - {i-7!-..... /,-- _ ! ! , '. l.i-.l.. ' . , . ! . , , ! , , .o .:,--
"- ........................., !/li//°_i ........... J.I I l _l-lL <LI ........ I .... L.JL.I i .... ii I 1 I I liJ l I I J,..Ti,,JLLL.I.J_L . i_ .l_LL,l
LL
t ," '"o_<><_,_,!._._.q _.o.oo._ _._ _._ _ _ _ _ _I I I I I I I I I I I
W33 'IN3131-_303 IN3ND_ 9NIH311d
!Ill_ , II I I ..................................... 1
1975006742-032
I_ i I
1975006742-033
L_
1975006742-034
1975006742-035
1975006742-036
J| I i II ill d | .....
1975006742-037
1975006742-038
i
J
"-- 1975006742-039
1975006742-040
..__ J
1975006742-041
I I
1975006742-042
r-- T .......I T IF "T -- - , -i
• i m
1975006742-043
........ ,_............ _.................. 7' "T, ''I
i I i
1975006742-044
I
_ '"• • o • • • • _
1"_ [1_- ('N
,-, O0
N .
z _ -_:
• ° ; I 7
: \\,£N _ I
0 ,,C ,.. _ _' _ ' I
.--, U-- I "_ Zn
........ Q_] c_ o_
CO O. _ O0
I
=J _ I " e "PO :7
; o
1-L--/._l_ ...l_i i i -.3. • I I i ¢ i I _ I i i i .
03'1N3131 -I-I3030¥_I0
1975006742-045
1975006742-046
1975006742-047
!i _',,._"._'l,Jl._I,Ji._.<.i_,]/i_ _j_l_ rl-r'T-T1-'rT-rn-F1-rT1-1r_il-ii_Tq-rri i 11r-I-I-1TTT1"-TT_T17" TT17_T I-T-TT .... I11, II'_14(,_
.....I('-_:_ ' _ "'h l.i ;
- ' I
_I_ ". _'-_,,,W o o I -_ UJ
_ oo _. "1_ 4C
.gF-
4------
....................._ ..........................l_h_ i -i o z
............................... ---J
I_i.J
_188 r , I } _
"< I !--mo_ , ' t'Y'l
.... , .... 1.........I......... I....
Q-] . _----T
_-_ I __ ('4 --4 0 _ O0 _,. _ It% _ _ ('4 _ 0 t_l I_L ,--,
88 ............. "q . _._<._,,_, - ._. _ , , %_#
N0 '1N3131-13303 33_I0-I 7VN[40N
III
1975006742-048
TI
• lllttirl Ill i#i
Z ll,. _i I'! i 1 ! ITI'T'I-I FFI"I"-'I-I-T'rT-I"-'T-I_T T-llr"l-l'-l-r'i 'l i i I i i I i l i i i i I I I '1 i I I i i i I' i I i I i i' ! 'T i i i i 17=l_.
ii'- _ .r,,I• , . . ° . • ill
0 O.
m ..ira x _- r,,_ln ! "CO
v-4
_ W
t_-- _ ,,. _ == •
i ,I 1 _ <>
_ t -J
_l_®® ,.-,o_ I.,-I,-- " ' "
L.LJ
,_ LJ_ .i I ,J.._l I 1 1 I L Ji I I I I i I I I I I i i ILI I I i l I l il I I I 1 I I I i I I _ (
NO °1N313I-I-1303 33N0-17VHI_ON
1975006742-049
1975006742-050
1975006742-051
1975006742-052
.................7,.......... 7 _ I' • - ,
1975006742-053
1975006742-054
1975006742-055
[ i
1975006742-056
• • ms • • _ m • •
1975006742-057
! i
1975006742-058
I
1975006742-059
i
1975006742-060
I
1975006742-061
i
1975006742-062
P" LAI hJ
._ L_._._Z_.___._ "('_'_:_L_'JFII'''III"|ITITIIIT1'IfT_TII'T'fTT'IITITTTrTT-TTXTI-rT-_TFTTtT1_I_T'T rT' T ,,TI , , ,T"T_._
•, t;_O00000
. - _,[)("_(7-- _ ....................................... r,,,
-. _,,k%o.o.q -
W N..,.mo................. 0
,., -IN
_ _ __ L,L LL J
(?_.('-:_I I I:Q |r_l j(]1x ;,-r4 5tI l
_J
• _ wJ • ' /L.! - _
,_ _j
.J
• . i " --J
; | z-' ";' (.3L '10 ' J <
>> .- ,_, . t,
................................. _0 W EZ_. _j H
- ' _ Z (---)
0:mm , ': I | ' i
g_o , I J <
"_ , _ .... . 1, , , , , , , 70 _ 0
.... EL
Y3 'IN3131__-_303 33_0-I 7VIXV
1975006742-063
• • • • mum _ • nu mu_u
1975006742-064
1975006742-065
r .............. _ ........ r r"--,,w ¸ T T _ ....
1975006742-066
1975006742-067
1975006742-068
1975006742-069
...........+ +.................... 7- T 'f ' "
° _ I/II,D_
+i..___ ,:_,,,.+,+,-,+,,....,.,-+,,.,+,+,+,--,+,_.+,.-,.T,,-.m,-.,+.+.m,,,-_+-,++,++_-T+.-_,_-,-:._--,,++ -+__8_,_,;;,_ -"
!_ _1. W
WW W L'_ rr _ <_
i _._. _
g+. ! _+<_+.+. _ : ._c_<
p" -,-, "I-
i _-'+
°+ , F }}x' i_: _ (.0 _
......... .....+ _ _+",'+,+,+, ' + ,+,+<,,,+,.- ......'............+......... +....... i "_ -+ "-- ILl
o:mm L..... -+.--..................... " _ w
_oo
_ iI! '"®_ ...................... I"%1
- ! ........+0. °,.,,U.J <:
- ,"* ,-' 0 0 0 0 0 0 0 Cl 0 0 0 0 (_7 0 0 _88 0 0 0 0 0 0 0 0 0 0 0 0 0 0 C) 0 0 U,,.J u.J.(NN ii • • I • • • • • • • • • • • • • u
)_:) '1N3131_-I_-130333_I0..-I30IS
III
1975006742-070
1975006742-071
• i _ • • n/ nu
1975006742-072
r ! _ !
! I
1975006742-073
I I i I
1975006742-074
1975006742-075
! l
m in o i Ill
1975006742-076
i
1975006742-077
1975006742-078
r I F
1975006742-079
1975006742-080
•r Y T
1975006742-081
1975006742-082
1975006742-083
Ill/
1975006742-084
.... r l
1975006742-085
.......... 7_ ' -'_'''w''_ -7 .......... _! .............. _ T
1975006742-086
1975006742-087
1975006742-088
1975006742-08'
L ' ' ' I ! - J- _ . ....... IIIIII i I l _
1975006742-090
.......1-975006742-091
.............T "_ ........I r_-- T T __
7
1975006742-092
T _T I"
i ! ,-,.i . ., - i ill
I i i ii i ii ii
1975006742-093
1975006742-094
.......... •'r.......... T .......... __'_"--"7
' 1........ •, . a __ - - -- -- • n n - -
1975006742-095
J
..... ' ' "_'" ' ' ' .... 1975006/42-096
1975006742-097
1975006742-098
1975006742-099
,. , I
1975006742-100
I__ I
1975006742-101
1975006742-102
1975006742-103
1975006742-104
, jL Ii mm _ i , , , i i I II il i ll • I I
1975006742-105
,
1975006742-106
....7 T V
1975006742-107
.... ! ..... --_t ............
1975006749-1_£
1975006742-109
1975006742-110
1975006742-111
1975006742-112
• I/I I/I _ I/I
_ _ I" r7"rI--r-r-tTT--FI--T-I--T----rT---r-FT--rTT-TW-T-rT-T T--t T7 -l--I r-r-;-T'-r-_ i I 1 l _ '_< . _ OD
-- "0 O.
_§II _ ; I i , { -:,"" _ ' t / / :' ...... --.................... --- --_w
,,i@, i -:7- II '. I ! ' P£.--7-2 ',./. : .-_,-
# _J
I 17. ¢-_
" /g ggg / /
IN0 •
--_ .:f El' _- ............ EL-"
,, _ T
_''_I_ _0 lid _I' _ 0 (_I ,_' (D O0 0 t'_ _ 1,0 _ ,--,_ I_I_I_ 0 0 0 0 0 0 0 0 0 .... W L_
r_ _ I I I I I I I I
W73 °IN3131_3303 IN3NON 9NIHDlId
1975006742-113
J
' 1975006742-114
1975006742-115
• III III IIII1_
-_--( .... o 0_,.,.
o • a " i I1'-t _fl_j i ILl
_!_!_ " ' ---" °_. "--'Ill
,--. " ' 0III ": .i
i * - 4!
i - -
f E' i"s
!_888. LL_
IN LI.-I
6 ggg ............ J_ ---_ m°
I ' IN- T
"_ "* "_ "* "4 "_ "-' 0 0 0 0 0 0 0 0 0 0 0_INPM • • • •
I
¥3 'IN31314-G0333a04 7VIXV
1975006742-116
}IA _ J n_TTT-V_TT11_TT_V_r_rT_TTTT-T_TTTTTT1T_7T-T_rT_y_TT-FTrT_T_1_T_T_tv_rT_
__•¢, "_ • • • " w
0 fl_
In .J_l] x _ _4J_
_ CO
o°° ,,_
--I
) <
!!I ' °_______ ! _ , I _
" '!I 1 1 ' -.... n
ggNg I _- I
•-. ,-_ .-, ..4 .... 0 0 0 0 0 0 0 0 0 0 0 L_J n
¥3 'IN3131-14303 33_0-I 7¥I×¥
k i , _l
1975006742-117
1975006742-118
b. _d rTIIITTl_rlITIITTT-TrlITtTTTrrlrT'TIrTTTtTrTrTTI,I-T3-rTFTITTTTTTT%_FT_T_ I_I-p_T _'l"
8 _ "_
................ "O 0W ....I_ bJ "
l :w _ W
"'" i WJ . tY
_g_ -
_ _ 4oI i
, _.J
I t..t._
§_ , ,,, I , o
_ _J
_ L.L_"-" _ _ *-_ "-" --_ .-' 0 0 0 0 0 0 0 r_ 0 0 0 _ L_
V3 '1N3131-I-1303 33_0-I 7YlXY
llllil
1975006742-119
1975006742-120
F .............. +,,. .......... _ • •
1975006742-121
1975006742-122
1975006742-123
1975006742-124
1975006742-12_
L ,, i i nlllnl nnnl ......... _ ._ . _ -- m . _
1975006742-126
1975006742-127
• dik_ -- I , ; , ,i , -£ • m m _+ _ i ,, ],,,
1975006742-128
1975006742-129
1975006742-130
1975006742-131
__J
1975006742-132
,m I
' 1975006742-133
7
1975006742-134
"-" 1975006742-135
1975006742-136
' ' 1975006742-137
1975006742-138
1975006742-139
i
1975006742-140
i
1975006742-141
1975006742-142
y .......... T ........ 7 T""'' _ •
_-lJ _W rr rf fl I Tllrl rlT_-ll-TlTrl l_ rf Fr i TT f I_TI-FT_ f-l-Tl-l-f l_l fTIT _-rl_l _ r _TYT r_
t,- _I<
"°'°°°" t_
tL I_1 "_-_LL J
- _ -LJ
• . o " k'J- _
'_tO•-4 LLI
- _ ("4 Ii O_
.. t-'-
----7" 7
<
g ggg I _ _
'I I ' * ' i _ '0 0jjj - .... I _ H
, I ,.L.LLI._ J.-LL._4 .I,-I,11_ L.LJi--L. J.J. 1J-L L.--LLLJ._ _ -L_LLI _LLLJL -L : _ _ _ _ k_ Lid
73 '1N3131-I-1303 I__17
IIIIIiI
1975006742-143
1975006742-144
1975006742-145
_-_,.,I_ _ P_'I-T-T [ T_I-I'-T_I-T I-I I I I 1 i I I I _ i t i [ , t : i I , _ i , _ I _ i ', * ._"_'_
(D
UJ ...... I',I
-
- .,"_ %_,
_ " ........ "_\ _'% ....... _. w
' ........................... \-% ................ .._, T
- I
L .... 1--- --_ ....... '-_ !.,.I I, : :_Y', .d '%_
L: LI
: F ............ i- ! t,J
t-" [ " k.L
. • CJ.._ ___. [ ',l t _) •
Fb'14k' k........ ,:
3
........... _ , • I I |_J_.
_I) If) U_ '_ _ 9- "L _ L,___: ,-,()( I"-If_l t _J • • • • I
'__k_ "'("! .....
II
1975006742-146
1975006742-147
r ..... • .... T r----,-,- 1
1975006742-148
1975006742-149
F !
1975006742-150
1975006742-151
1975006742-152
_ _1_ J _[! I| TT I"1"I 1| 1! I .... 17 qr T'I f • _ T-T-FT-r'T-TT'TT I_7_T-T' T'TT-T1 Tl7 1 T 1' FT T-T'I_FT T_I- TT
• • . . ° o . W
" I [i,l...
Lul_0 I UJ
Id - • . |
w [ , _' C")
_t_ _0 _--
-_' _ _ 1 -ii -Jz _,,-.--_Z
1888 r......... -_ " --_- ' O_
t r _ 4 _j
it. ' ' ' ,,., "n._.._. ._.. o o
;.___ r ,_ _ c_ •
JJJ E+_
CI.],0, F (_J u)" LILL_LJL ll_ It 1_ I_1 I J. 1J tJ lJ- J++J[ I _ I I [JIJl I I I I _L-LJ..-L LLI (
' ' • LI._ _F_ m-..,- t/') 0 IS') 0 U') 0 IJ1 O I_ 0 I/1 0 If) 0 If) h_ ,-," _Bfi ............... w o
0/7 'OllV,_9V_I0/1-I17
II!IiI
1975006742-153
:
1975006742-154
1975006742-155
i
i
1975006742-156
1975006742-157
r ............. _ ...... .... [ ....... _ ] T
P- u]wwl,|w T-'T_.i
_k _r.._'IJ I'[Tr]FT-IrrI*IrI_WI-IFTI--T_-T-TFT'II1TTI-I-T-;I T_ r! :T-FT-FF I _FT-I-T-rT-T'T-_-_..,_,_,_,,.<_ . o_
(N
- - i 0 CL
b.l
bLL_tL J
UI _lm x _mN6'9
. , I W
'" i ........................ _ ..................................... ----_W" C3
-J i i _ !
' . $, 1 : 0.
_I_l_ , _ I _ -'..... , .......! ......_ L .................... (.j Z
,_ _. ......___.......:..........................m__. i--, _ t i t_. _:_
" k __._1
1 °, _j rr."
! i 2j.l
_ >- /'"i I I !_1 _21
g 74g_ _ I _w
W 0.,..,r ._>>" ......... _.... _'t "_.............. ............... - (..) [_
t o
_-P-v- .- -..........'i i........ --I"-........_<<< , ....._ .! ._, 7 ,,_ono " /'-'_ I '
">_ l " I l - <_,_o_ O0 ¢0 I'.. ¢'- r'- r-- r'- ,<;,),._ or, to ,:._ _ iF) u') > u
*¢ ;'_ r-J P-J N • • • • el i _ * _ • • • • •
7/d3X 'HIgN37 1008 NO (23SV8 bIO:'.LVJO-I71_flSS_Nd --JO_131N33
1975006742-158
1975006742-159
1975006742-160
1975006742-161
_ k* J r[__J r i i 1 i 1 i i { i l I I I I I [ i 1 I I I l _ [ I t I I ! I'll I f Wi-TT I-I-l"I rlr i rl Irl-[1 f'I
}I, ":e_? i,i- C:,_)(>,_ " I,IJil - * ° •
cA _ ii:
"" - ........................ • ............................ _ ------'-_ I
/
°" Ui : i i y i :
. I i ' i : : _ _ I.L I_i
- _ _ i %." i i I I ID ----I........ Ill
-: i ! ! , 0 "• ' , Z O0
,, . ! ., , i )3".$ : _- LLI
--" ill _ I i :
" ' i_; _ i- -:- ' '.........:_
i' . r I i i I
; { I ! E)
,,:t i ' i I _ --
,; r (..ll) r-- _ 7- ! • _ ci_ ,.CJ CD ,O CO lri i_ if) > cO
'lidSi× "IIL_.'JN:J _ .;,,,{{{ I'll) ilJl')','Et t.!f.]llVDiTli ]tT.FISSJb<.t JO N]IN__3
1975006742-162
I W'
• i
1975006742-163
1975006742-164
1975006742-165
1975006742-166
r ]
. K,1, i_l/i u.i
_i • .| jil..i I,.i (_) l( ri i t 1 i ! ! 11 1 i i i r 11 - I f r-i i rTrrT-TIT_F__ N-H 1_T1-'I'-I'1 I I I I I ii_iloo
- o ' .r-:,,{_ . w1_:-,: " . ->__
_'_ :,.>. 5_t" t' "- ,.; - " ./ ...... ............... I%1 13_
- o
'_---_ -.., - ..........................
' "_00 <:
, I---
" O I-_
:., h_i ___, _lll ,,• < C) .......... ,-,--
.........'-' L _4..___,....! .....L--_ ___._____ --ii" u._
:_ _! >.
,m, _" I " c.)
'- !-7 t_ k i ......... I_.......... !,, ,.i___L__ _l , , _ I_
0 _-_ 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 W0 0 0 0 0 0 0 0 0 0 ¢) 0 0 0 0 0 0 0 0-
0 0 0 0 0 0 0 0 0 0 () 0 0 0 0 0 0 0 _)
',4_{TdS{i/b_OC_. "_.".-i0 9_V_8 033d0 / 1N31317_303 IN-_gN 9NIHOAId NI 30NVH3
IIII
1975006742-167
I
_1. _J rl I I T I, T | i I T ! I I- I s W I I T T T- _ _ I _ ( | 1..I I _, ; | I [T_I | | f FTT -I- l~_.l-T.._ l _ r-T Y I FT-[ I--T-FT-] l'_
-- Bzzzzz B - , .-
-
i ......\ I0
: II : : ,," ./" . : ! I L.d
i /! iz _ _ I ,_1 i ! 1"_ I , I I j.l I I I ! I "lm <
., -_" _ i i i T i i _ i_,---_°
:........... 1..;:,_ ..... i. _....i:-- _---._f,..... ..... i -- .... r ..... ' ......_-.... L..... ,--.-; -7r_ _ _ ' _ ' , ,./'-I I .Y , _ , I <J , I
'_, _. _= t _ ! ' /f' !./O u i : : p,.. .L_ I : ," , i I , } i t _ ! ,t'.,i
< _ i.. ; _ \ 1\ I /- ; i / | I } , J z
_ o:-" _- , I 4" '-' t t I , c_,
"_i", ...., _ EL_I ; !
_ _ d _ _ _ ! t I i i i....... .......... [ 't ..... '_" " -- .... !]" I------------'--''_}' '_'-- - ' ' j __ U.JL_j
Or3
C) F__' _.') =) ',i_ C3 :) C3 0 0 0 0 0 0 0 0 0 0
0 0 0 0 _D C) C._ Lm 0 0 CD 0 0 0 0 0 0 0 .m(.)L JC; 0 (z), 0 O_ C_, 0 cb,. _ C)o C.J, 0 , O, ;--3, O, O, O, O, O, td_
:ddSdtO,/I,4i:)f} "' .{]tl} ::_,_.¢,,"tJ8rt-j?,,_b ' .Lt',llS_J'OI.:l..:l'--J03.N_140_,_9NIH3JId NI 39NVH3
1975006742-168
APPENDIX
TABULATEDSOURCEDATA
Tabulationsof plotteddata are availableon requestfrom
DataManagementServices.
!I
1975006742-169
r ..... T........ r _ "T "
o
_ _ • • • ,. .... • • ; ,. •;. , _ • • ,. ,. ,......... ,.
.............. _ _ ........... ,,;,,
_ _oooooooooo°_ ..............
_| _ ,,_oooooo_o_. ...... ,, _ ..............
_¢_._ _ ___,_R_
_ ,_ , _ '
...... ___ __oo-__
II II II II
I!
1975006742-170
_ _o_o_,_o_ .q . . . _ ............. •
|........... _'''*i'i'101"iiiiii
.... N_ _ _ j _0000000_000__000
000000_000
0___ ..... _ ........... i'10o
00 _ _ G .......
_ _;; _ ..... _ , ...... .£ $$$___
_ _ _ o _o__ _..... _ 6 °°__R_R_...... ,
_ _ ............ t ...........II iI II II
llllli;'i
I
1975006742-171
1
o°.
II II I! J • - • • • • • , .... _ • ......
._ . ._ . , .q _ ._ .....
I_ 8. d , ,............ . _q_ C_ .=, , ........
. _ _!_i_i_'_ _ _,_,,__°_ _ _.......... qq T _ . .:2 . .- ......T _ o|111_1 *111| I
_,,oo° .... .°o _ ...........
i_ g g
.............. qqq .....N
°
• • • o ........ _ ..........._ ,,°.o _ _
I! II _1
N _ _o_e_o_ z_ ..........
• 0 . o
II I I
1975006742-172
t
f!
| I J I I I I
. • ......... __...
qqqqqqqq£q£qqqq _q_qqqqqq_q_qqq
g g _ _
i _ i, • .... • .........
............... O0 0 oI1_ IIII
# ii ii
Az
,. • • ............ _ g nq qqq I_ _ _ 9 _ _ _ qc?
$o I g
........... .., o.... .........
m
1975006742-173
O0
...... _ ,' ," "_46_ " _ _ ," "_6__6 "
,,,,,, _ _ _ _.__ _ _o_ ................ o _,,'°'°°°''°°'°°
T _ ..............................
° _ ..._._...__ _ _ ...............
_ _ _...___. _ _...__..._
_ _ _ 5 ............... 5 .. .. ............9 _ _ ' _ ', t! it
_ _ _,.,- ............. _ _ ...............
...... , ...... ° _ .... ° 0 ....... 0 _
II
i i i
1975006742-174
I
• I
000
_ ............... B _ ...............
_ ........
, _ ............... _ O ...............IIIII I Ill I
0 •J
i'ig ii i ""0___ _ _ _ _h_
_; _ ..............................Ill ii
II " • ...... • i_ i_ i° 1_ i° 1_ .... • ° " " I" I" I" I" I° I° _"
.... 0 • • • • ........... _ • o '0 ......
• 0 • •
00 .... • .... °0° _00°,00° .... 0.,
o
_ gSgg
1975006742-175
000
_88
0 ............... _ ...... "°°''°°
_ ... .............
8 d_qqq_ ..... e_oo d_;g_ S. ,,, " ..... _.:" 8 ....
° _ _ ....__ _ c___.
. _ _ .........iii iii1 ii _ |
qqqqqqqqqqqqqqq _ _oo88_o888oo8°
_ ° _
|1 • ° .......... - • . ,i .............I11111;iii iiitt111
I I II I I
g 2 $_,
, • , °1
_I .............. _ ............
II II Jl
II
1975006742-176
• ° °
_ m
- _ _gSB$8_8
_ _ _ _.............illllllll
. ° .... , . • ....
II II
= ._l_
1975006742-177
IIFr ............ _r...... _'T r ''..m _'m''-''_ ]
, • .
_j ............. J ..............
i| t
_o ,_ • .,(
• _ 8 _' ," ,"'" ........... _-; ," " ..........
" ,- ,_ -. :, . • o ._-t:,_._L "_
g _
•_ _ ,., ...... L:; °; "q " 8 _;_j ............................
" _ _ -_-"_,, _.._.........,..:_"_:_ _ :_£_:_,i_:'____ __ _..oN
_P
ii .......... t2
e-
@... ,,.,
_" } _' ,. ,........... .: • __ _, . ,.......... _; .
• ._ _g_ _ .....
" _ 'I. .... _.,'.,: q -: ,: - ,: _ ": .... - . . . ¶ .i,I
_d
11
1975006742-178
...._ ..... T....... _ _'-T ''_'- T_ ?
i m i
1975006742-179
.'
!
• •
• , ° ....0 , , , ..J ............ J _-- ' " _- AJ N
i," v_ P- P* r- ,-_ I,-L" •
g e_ .':': .................." _ . _'_.
:._ C, .......... _") C ............
i _ g g
._ g _I . .: _.?c: .................
_
- " ........ I A . 2 ,_.:2 ._2 2 2
1975006742-180
ill"'IIIii
1975006742-181
j ......... ._ , . ,
° .,_ •
I! II le J .-,, _ ¢3
II II
i ,.- _ g
N _qqqqq qq qq L!q £ _.q _ q _.q q _ qqq q q q q q qI I I I
o _
(,._ • • o
r I_ Ii
• o ° -- ........................
Id
1975006742-182
IIp" ....... .............. _ ..... " --'-_l" "" - l _ t "T
t
qqq
j_ ...........0 ,
.. _ ,
o _ _ .......................
_B o ,, _ .
o _ _qq .......... G ...........iiit iii i
_o _; ............_ ...........
g _ 8
_ _ _° _ _ ._ ................ _q . u "
- _ _" , ............. _ , ....
= _ _ _ o _._._._._ .... _ ...........
_" _ ,'g#4_Adddg5 .... 4 ......
........... _g_gj;ggg_g
_,_b_
Illiil;
1975006742-183
I
It II 0a
• -. _ ..... _._..._ ____......... .....II II II
. , .'.q ......... _ _ ...... q .R .... q
,o,o, ....... ,o .oo, ....... ooo
E _ ____ _...,_.._..® _ _ ............. _ .............
.... o • , • • ..... _ , ......... o • .II(llllllll /It IIIIlllll
0.oo
• • ......... , • _ .............
• _ _ .............
o _ |1 ii ii
I III - - III -- - II [
1975006742-184
1975006742-185
II II II
_ g
tII II II
-_ ............ . _!!!!!!!!!!_
: ............ :_!!!!!!!!!!!_ _ ! _i__ _ _ .o..°_..o._ IIIIIIIIIII iiiiiiiiii
o _ ..... ._ _ _ _°°..,° .....
* i I I II IIIIIiiiiii
i llillllll
_ _ ___ _
_ _Sgg
1975006742-186
k_
1975006742-187
II.... J
1975006742-188
'............... 1 ....................... i ........................1-............. 1 .................. 1 .................... v ........................_ .......... !
ji 6_ r:
_ ._ _ , ._ . ._ .qq_ ...._£ _ _ ...............
,, _.,_'_,_ _,o_ ,, _ _ _ __ _ __ m_ _ _ ..... £ .£_ .....
#11)11111111 I
# _ iiiiiiitt11111 illlllllllllll
Ii. _ ............................
i
7_ f .............. _ ..............
IIII"; il
1975006742-189
° • o
Of el Io
_ o
_i _ _!!!!!!!!!!!!!!! _!!!!!!!!!!!!!I| II iI
8_8e _
_i_°°-' _!!!!_!_!,____ _ __ _-_lll_ll!_lllll..._.........
'i :_!!!!!!!!!_..!.._ _!!!!!!!!!!!!!
b _ ," o" ," ," ," ; ," ," ," ," ," ," ," ," " ," ," ," ," ," ," ," ," ," ," ," ," "
o _ _ ..... __,_ _ _._._.._:_
_ o _ o ooo,o_ _.............I- i'lll, l,l'lll=lOlll, lll'l,l I. _ iiiiiiiiiiiiI
II II II _ i I #
_ t .............. t ............
._
I
19750067;_,2-1.qn
,l , ii
_J
G
ir jj j
o
_ _; _ ..............._ g _5
m
......... '2 . . _..._r
_ _ ........, , , , ,' • ,. . . . . . ,.
Z J ' ' "
I i ii I IIIIIIII
1975006742-191
'T ....... _ v............ ] T "
• • °
I_ ii it iiin
0 v
,.. "._" g .......... ,_,-'..,-"._. _i_ ..... _..... ,:t '
,_,.J
i i -i
_,_ _,., .............. _,., ..............
................ ........ __ ,:.,:.._, ............. _ .............
- _o ¢_ • • • • ; • • • • • • • • • ,_ _.,• .............• i | i i i i i i ! ! i i i i _ i
_ - ...............° ...............,_ ° ° ,
t ............. t .............
0 9#
" II
1975006742-192
,Jr
: Ll
II
LI B
g _ g
"m _ ............. _ ............J _ _ .. ....
• ._! . , N. ......_ ,,I. . _ _ . . , _. .........
,_ _ _ ..........................J "J " " " L_
.t _ • :
"_,_ _ ............. ! ............
,-' _,.__ :_
IIII! 'IIIII1'
1975006742-193
• . .
0 ii ii i*
; _ rJ70 V
_ o
_ i* i I i" i* iI i* * i* i* i* i* * -. 1" " , i.......
_ _ _; ........
, ,_i_,,,,_:-_ !i!_:!_._:_i_ ....... _, ...............
. -" _II ......................
_ ........... _.2.2,1,2.:,2.'.2.2.J
Sgg_
IIIJ
1975006742-194
N _
_ jj II If
0 _
_ ,
_£qqq qq£qq£qq_ o g S
_ .
_ _88_ 88 88_ _ So
_ J o .qq .q ._. • ,£ .q ................
g _
_ M .......... 0°-0 00o° ..........m L; _ ............. _ .............
......... _ ° 0 • •r _ ._- ..........
lllilllllllll llililllli_ll
0 • • •
t ............. _ .............
_ -_:
ii II II II
1975006742-195
.££
_ ....................... £Nqqqq
,_ _ .............. _ ......... _.._.
_ °'°°°'''°*'.°" .... ,...,.°...
''''''''''''' _ '' _ .... ,,,,,,
"°*****°**'*°* _ i'''°'''*''°**.
5 _ ,,,,,,,,,,,,, _ ,,, ,,,,, ....
Illl|llllfll IIIl,lllltlll
_ • • .
.... . _' _;_o__ _
_ ............. t .............
i I I I
197500674P-1_Cl6
.R£
z
II ii
_ U
,__._.._ _!_°!_°_°_o___o ,_i__!_o_o_ ot
II II II
u • • ..... • ° ' • ° U ° " .... • ° • ° °
_ •
._ooooooooo 87t 8t8 l
_ _ ........... _ ..... , ....
............. • o • ° • , ° • • .I IIIIIiiii IIIIIIIIitl
...... °o ............ °,.b _ _ UIIIIIIIIII I _ UIIIIIIIIII
1 ........... f ..........
I°• • ° _
# II II II It
" _5gg
_L
- " II1975006742-197
