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J- A
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COMPILATION OF CA t lBRATIO'N7 :FOR AEROBEE FUGH 3'-GP-
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https://ntrs.nasa.gov/search.jsp?R=19650009335 2020-07-27T09:04:28+00:00Z
.
COMPILATION OF CALIBRATION DATA
FOR AEROBEE FLIGHT 4.13 GP-GT
BY
L. C. C a s t a g n o l a
N a t i o n a l A e r o n a u t i c s and Space A d m i n i s t r a t i o n
G o d d a r d Space F l i g h t C e n t e r
SuMlldARY
An Aerobee 150A. des ignated F l i g h t 4 .13 GP-GT, w a s f lown
as an Aerobee performance v e h i c l e and w a s h e a v i l y instrumented
by personnel of GSFC's Sounding Rocket Instrumentation S e c t i o n .
This document c o n t a i n s a compi lat ion of c a l i b r a t i o n d a t a and
curves for instrumentat ion aboard t h i s r o c k e t . In a d d i t i o n ,
payload te l emetry channel a l loca t ions , p e r t a i n i n g t o t h i s re-
p o r t , are a lso contained.
i
c
TABLE OF CONTENTS
SUMMARY i
TABLE OF CONTENTS ..................................... iii
L I S T OF ILLUSTRATIONS ................................. V
L I S T OF TABLES ........................................ v i i
1 INTRODUCTION .......................................... TELEMETRY REQUIREMENTS ................................ 1
CONCLUSION ............................................ 2
...............................................
iii
LIST OF ILLUSTRATIONS
Tit le Figure Number Page
7 1
2
Accelerometer Frequency Response Curve ...... Accelerometer Assembly 1065 X-Axis (S/N1121)
Calibration Curve ...................... 8
3 Accelerometer Assembly 1065 Y--Axis (S/N 1063) Calibration Curve . . . . . . . . . . . . . . . . . . . . . . 9
4
5
6
7
8
9
10
11
12
13
14
15
16
Accelerometer Assembly 1065 Z-Axis (S/N 1003) Calibration Curve ...................... 10
Inside Temperature Aft (S/N 44895) Calibration Curve ................... ...
Inside Temperature Forward (S/N 47839) Calibration Curve ......................
11
12
Fuel Bottle Temperature (S/N 47830) Calibration Curve ...................... 13
Aft Helium Bottle Temperature (S/N 44878) Calibration Curve ...................... 14
Oxidizer Bottle Temperature (S/N 44896) Calibration Curve ...................... 15
Fin Cuff Temperature (S/N 48792) Calibration Curve ...................... 16
Tail Can Bulkhead Temperature (S/N 48794) Calibration Curve ...................... 17
Helium Regulator Temperature (S/N 52316) Calibration Curve ...................... 18
Forward Skirt Helium Bottle Temperature (S/N 52313) Calibration Curve .......... 19
Coolant Outlet Temperature (S/N 44893) Calibration Curve ...................... 20
Coolant Inlet Temperature (S/N 44894) Calibration Curve ...................... 21
Gas Regulator Pressure (S/N 11081) Calibration Curve ...................... 22
V
Figure Number
LIST OF ILLUSTRATIONS (con't)
Title Page 17 Helium Tank Pressure (S/N 7411)
18 Fuel Gas Line Pressure ( S / N 11081)
Calibration Curve ...................... 23
Calibration Curve ...................... 24
19 Fuel Line Pressure (S/N 11474) Calibration Curve ......................
20 Oxidizer Line Pressure (S /N 11086) Calibration Curve ......................
21
22
23
24
25
26
27
28
29
30
31
32
33
34
Oxidizer Injector Pressure (S/N 11090) Calibration Curve ......................
Fuel Injector Pressure (S/N 11093) Calibration Curve ......................
Fuel Coolant Inlet Pressure (S/N 11094) Calibration Curve ......................
Fuel Coolant Outlet Pressure (S/N 11089) Calibration Curve ......................
Chamber Pressure (S/N 11088) Calibration Curve ......................
Booster Pressure (S/N 12529) Calibration Curve ......................
Lateral Magnetometer (S/N 401) Calibration Curve ......................
Longitudinal Magnetometer (S/N 404) Calibration Curve ......................
25
26
27
28
30
31
32
33
34
Pitch Ogive Calibration Curve ............... 35
Yaw Ogive Calibration Curve ................. 36
Solar Aspect Sensor, Model 133E Code 37 Reference Diagram ......................
Solar Aspect Sensor., Model 133F Code 38 39 Adcole Models 133E & F Grey Code Pulse Train .
Transducer Orientation , 4 0 v i
Reference Diagram ......................
Table N o -
LIST OF TABLES
T i t l e Page
1 FM/FM Telemetry System Frequency and Band A l l o c a t i o n s ....................... 3
2 I R I G Band 13 Commutator Segment A l l o c a t i o n s . 4
3 IRIG Band 10 Commutator Segment A l l o c a t i o n s . 4
4 PPM Telemetry Systems Channel A l l o c a t i o n s ... 5
5 SST I 1 Channel 15 Commutator Segment A l l o c a t i o n s ............................ 6
6 Code Table for Adcole Solar Aspect Sensors Models 133 E & F (6 s h e e t s ) ............ 41
v i i
. 4
INTRODUCTION
COMPILATION OF CALIBRATION DATA
FOR AEROBEE FLIGHT 4.13 GP-GT
This document p r e s e n t s a compi la t ion of c a l i b r a t i o n data and c u r v e s for i n s t r u m e n t a t i o n flown on Aerobee 1 5 0 A . F l i g h t 4 .13 GP-GT. Launched from Wallops I s l a n d , V i r g i n i a on 26 September 1964, F l i g h t 4 . 1 3 ' s payload c a r r i e d p r e s s u r e and tempera ture t r a n s d u c e r s , solar a s p e c t sensors , magnetometers, and a pitch-yaw ogive. C a l i b r a t i o n cu rves and d a t a (F igures 1 through 34) a r e s u p p l i e d so t h a t t h e expe r imen te r s can reduce acqu i red raw data .
Primary o b j e c t i v e s of F l i g h t 4.13 GP-GT w e r e t o g a t h e r e x t e n s i v e p r o p u l s i o n data on t h e Aerobee 1 5 0 A , as w e l l as v e h i c l e environment da ta ; i . e . , t empera tu res , p r e s s u r e s , and a c c e l e r a t i o n .
TELEMETRY REQUIREMENTS
F l i g h t 4 .13 GP-GT c a r r i e d one FM/FM t e l e m e t r y system ana two Pu l se P o s i t i o n Modulation (PPM) t e l eme t ry s y s t e m s f o r data t r a n s - miss ion . The FM/FM s y s t e m conta ined I 3 s u b c a r r i e r f requency bands a l l of which were a l l o c a t e d t o in s t rumen ta t ion . Table 1 .provides a breakdown of I R I G f r e q u e n c i e s and a l l o c a t i o n s of t h e FM/FM t e l e m e t r y s y s t e m , which w a s modulated on a frequency of 256.2 m c s . Tables 2 and 3 provide segment a l l o c a t i o n s of commutated I R I G bands on t h e FM/FM t e l e m e t r y system. I n Table 1 n o t e t h a t I R I G band 14 w a s a lso commutated, bu t s i n c e data on band 14 does not p e r t a i n t o t h i s r e p o r t , segment a l l o c a t i o n s a r e no t l i s t e d .
The PPM t e l e m e t r y s y s t e m s w e r e de s igna ted as SST I and SST 11, t r a n s m i t t i n g on f r e q u e n c i e s of 240.2 m c s and 231.4 m c s , r e s p e c t i v e l y . Each PPM s y s t e m con ta ined 15 channels , which were a l l o c a t e d as shown i n Table 4 . N o t e t h a t Channel 15 of SST I1 w a s commutated. Segment a l l o c a t i o n s f o r Channel 15 are provided i n Table 5.
TEMPERATURE AND PRESSURE SENSORS
Temperature and p r e s s u r e s e n s o r s , flown on Aerobee l '50A F l igh t 4.13 GP-GT a r e d e f i n e d and l o c a t e d as fo l lows :
- A f t Sk in Temperature; measured s k i n tempera ture of a f t s e c t i o n of s u s t a i n e r and w a s l o c a t e d on t h e under s u r - f a c e of shroud 111.
Ts2
- Forward Skin Temperature; measured s k i n tempera ture of forward s e c t i o n of s u s t a i n e r and was l o c a t e d on t h e under s u r f a c e of .shroud 111.
Ts 1
- Fuel B o t t l e Temperature; measured tempera ture a t t h e f u e l t ank and w a s l oca t ed under shroud 111. Tf b
1
- Thr
Thb 1 -
Tco -
Tci -
Aft Helium B o t t l e Tempera tu re ; measured t e m p e r a t u r e of t h e a f t s e c t i o n of t h e he l ium t a n k and w a s l o c a t e d under sh roud 1 1 1 .
O x i d i z e r B u t t l e Tempera ture ; measured t e m p e r a t u r e of t h e o x i d i z e r t a n k and w a s l o c a t e d under sh roud 111.
F i n Cuff Tempera ture ; measured t e m p e r a t u r e of f i n I11 and w a s l o c a t e d on t h e u n d e r s i d e of t h e l e a d i n g edge of t h e f i n c u f f .
T a i l Can Bulkhead Temperature ; measured t e m p e r a t u r e i n s i d e t h e t a i l c a n and was l o c a t e d between s h r o u d s I1 and I11 on t h e a f t bu lkhead .
Helium R e g u l a t o r Tempera tu re ; measured t e m p e r a t u r e of t h e he l ium- fue l p i p e and w a s mounted on t h e p i p e .
Forward S k i r t Helium B o t t l e Tempera tu re ; measured t h e t e m p e r a t u r e of t h e he l ium t a n k i n t h e fo rward s k i r t and w a s mounted on t h e t o p bulkhead of t h e t a n k .
C o o l a n t O u t l e t Tempera ture ; measured t h e t e m p e r a t u r e of t h e c o o l a n t o u t l e t i n t h e t a i l c a n and w a s mounted on t h e c o o l a n t o u t l e t p i p e .
Coo lan t I n l e t Tempera ture ; measured t h e t e m p e r a t u r e of t h e c o o l a n t i n l e t i n t h e t a i l c a n and was mounted on c o o l a n t i n l e t p i p e . Gas R e g u l a t o r P r e s s u r e ; measured t h e r e g u l a t e d he l ium ups t r eam p r e s s u r e of t h e check v a l v e i n t h e r e g u l a t o r .
Helium Tank P r e s s u r e ; measured t h e p r e s s u r e f rom t h e he l ium b o t t l e i n t h e r e g u l a t o r .
F u e l G a s L ine P r e s s u r e ; measured t h e r e g u l a t e d he l ium downstream p r e s s u r e from t h e check v a l v e i n t h e r e g u l a t o r . F u e l Line P r e s s u r e ; measured t h e f u e l f l ow from t h e f u e l t a n k i n t h e s u s t a i n e r .
O x i d i z e r Line P r e s s u r e ; measured t h e p r e s s u r e of t h e ox- i d i z e r l i n e and w a s l o c a t e d i n t h e t a i l c a n plumbing.
O x i d i z e r I n j e c t o r P r e s s u r e ; measured t h e p r e s s u r e of t h e o x i d i z e r i n j e c t e d i n t o t h e t h r u s t chamber.
F u e l I n j e c t o r P r e s s u r e ; measured t h e p r e s s u r e of t h e f u e l i n j e c t e d i n t o t h e t h r u s t chamber.
F u e l Coo lan t I n l e t P r e s s u r e ; measured t h e p r e s s u r e of t h e c o o l a n t i n l e t f u e l t o t h e t h r u s t chamber.
F u e l Coo lan t O u t l e t P r e s s u r e ; measured t h e p r e s s u r e of t h e c o o l a n t o u t l e t f u e l t o t h e t h r u s t chamber.
Chamber P r e s s u r e ; measured t h e chamber p r e s s u r e i n t h e t a i l c a n ,
B o o s t e r P r e s s u r e ; measured t h e b o o s t e r chamber p r e s s u r e and w a s l o c a t e d on t h e b o o s t e r ' s forward bulkhead .
CONCLUSION
This document i s a pre l iminary i s s u e for r a w d a t a r educ t ion . Documents p e r t a i n i n g t o performance i n s t r u m e n t a t i o n e n g i n e e r i n g and i n s t r u m e n t a t i o n f l i g h t a r e forthcoming. The i n s t r u m e n t a t i o n performance eng inee r ing r e p o r t w i l l d e t a i l t h e eng inee r ing r e q u i r e - ments t o p rov ide p r e c i s e a c c e l e r a t i o n , t empera tu re , and p r e s s u r e dev ices . F l i g h t performance r e p o r t s de ta i l t he background of t h e payload i n s t r u m e n t a t i o n ; personnel p a r t i c i p a t i n g i n t h e program; d e t a i l e d d i s c u s s i o n s of t h e experiment , t e l e m e t r y , i n s t r u m e n t a t i o n . and o t h e r payload areas as a p p l i c a b l e ; t i m e r sequences ; i n t e g r a t i o n o p e r a t i o n s ; and f i e l d o p e r a t i o n s .
2
Table 1. FM/FM T e l e m e t r y System Frequency and Band Al loca t ions
I I
70 kcs i 18
52.5 kcs I 17
16
15
40 kcs I 30 kcs !
22 kcs
14.5 kcs
10.5
7.35 kcs
5.4 kcs
3.9 kcs
3.0 kcs
2.3 kcs
1.7 kcs
14
13
12
11
10
9
8
7
6
ALLOCATION
S o l a r a s p e c t in format ion
Accelerometer X -Axis
Accelerometer Y .Axis
Accelerometer Z--Axis
Commutated (not provided i n t h i s
Commutated (see Table 2)
Sodium Hot oven
Sodium Cold oven
Pb, switched t o commutator a t
T +3 seconds (see Table 3)
r e p o r t )
Nike valve moni tor , swi tched a t
T +3 seconds t o ACS r o l l p o s i t i o n
H e l i u m Regula tor Temperature (Thr
Forward S k i r t H e l i u m B o t t l e
Temperature (Thbl)
Coolant Outlet Temperature (Tco)
3
Table 2 . I R I G Band 13 Commutator Segment A l l o c a t i o n s - _ _ _ -- SEGMENT . - . 1 ALLOCATION
I . 4
2
3
15. 6 . 11, 1 2 , 1 6 , 1 7 , 18 ,
122, 23, 24 (c ross -s t rapped)
7 , 8 , 13, 1 4 , 1 5 , 1 9 , 20 , 21, 25, 26 (c ross -s t rapped)
' 9 , IO, 27 , 28 (c ross - s t r a p p e d )
29. 30
' Ground
2 . 5 v o l t s c a l i b r a t i o n l e v e l
5.0 v o l t s c a l i b r a t i o n l e v e l
Y a w og ive
P i t c h ogive
Tip e j e c t monitor va lve
5 -vo l t p e d e s t a l (sync)
Table 3 . I R I G Band 10 Commutator Segment A l l o c a t i o n s
SEGMENT
L , 2 , 131, 92, 13 (cross -s t rapped)
3 , 4, 14, 15, 1 6 (c ross -s t rapped)
3 , 6 , 17, 18 (c ross -s t rapped)
7, 8 , 2 0 , 2 1 , 22 (cross - s t rapped)
9 , 1 0 , 23 , 24, 2 5 (c ross -s t rapped)
19
29
30
ALLOCATION
I n s i d e Temperature Forward (T ) s l
I n s i d e Temperature Af t (Ts2)
Aft Helium B o t t l e Temperature (Thb2)
Fuel B o t t l e Temperature (Tfb)
Oxid izer B o t t l e Temperature (Tob)
Ground
500 ohms c a l i b r a t i o n l e v e l
1100 ohms c a l i b r a t i o n l e v e l
4
Table 4. PPM T e l e m e t r y Systems Channel A l l o c a t i o n s _-
I ALLX)CATIONS
CHANNEL
1
2
- _-
3
4
5
6
7
8
9
10
11
12
13
14
15
SST I
G a s B o t t l e P r e s s u r e (P
G a s Regula tor P r e s s u r e gb
gf2) Fue l L i n e P r e s s u r e (P
gf 1) G a s Line P r e s s u r e (P
Fuel Coolant I n l e t P r e s s u r e (Pfci)
P r e s s u r e (P ) Fuel Coolant Outlet
f c o F u e l I n j e c t o r P r e s s u r e
(Pf j)
Chamber P r e s s u r e (Pc>
Oxid izer Line P r e s s u r e
(pol)
SST I1
High Energy R a t e Output
Low Energy Rate Output
High Energy Rate Output
Low Energy R a t e Output
High Energy Rate Output
Low Energy Rate Output
High Energy R a t e Output
Low Energy R a t e Output
High Energy R a t e Output
Oxid izer I n j e c t o r Pressure1 L o w Energy R a t e Output (Po 1 !
Load C e l l A/switched t o ' Long i tud ina l Magnetometer ACS a t burnout
Load C e l l B/switched to ACS a t burnout
Load C e l l C/switched t o ACS a t burnout
Load C e l l D/switched t o g- reduct ion t i m e r a t burnout
Coolant I n l e t Temperature (Tci)
Lateral Magnetometer
High Energy R a t e Output
Low Energy R a t e Output
Commutated ( see Table #5)
I i i I
i I I
I I i i
I
I I I
I j ! 1
I Channels 2, 6 , 10 and 14 were c ros s - s t r apped t o i n c r e a s e frequency response (SST 11).
5 I - .-
Table 5. SST I1 Channel 15
SEGMENT
1. 4
_-
2
3
5 , 7 , 11, 13, 15, 17, 19, 21, 23, 25 (c ross -s t rapped)
6, 8 , 1 0 , 1 2 . 1 4 , 16, 18,
,20, 22, 24 , 26, 28 (c ross -s t rapped)
i
Commutator Segment A 1 l o c a t i o n s
ALLOCATIONS
30
27
6
150 ohms c a l i b r a t i o n l e v e l
100 ohms c a l i b r a t i o n l e v e l
50 ohms c a l i b r a t i o n l e v e l
F i n Cuff Temperature (Tfc)
T a i l Can Bulkhead Temperature
Ground (Ttp)
50 ohms c a l i b r a t i o n l e v e l
130 ohms c a l i b r a t i o n l e v e l
Open
+
I '-
>. U Z 3 U W
W ' 200 fE
100
80
60
40
20
10
8
v) +
2 +
(Y
+ 7
43 +
0
P
(Y
I 7
10
h VI
3 Y
a, > L
d C 0
m 0 0
Z . \ v, v
Ir) 9 0
L 3 zn .-
LL
al L 3 C 0 .- c e e - s n
Z \
2 3 c
2L E al I- S Y tn
.-
!!
ii 3 tn
(SWHO) 33NVlSIS3Y
11
h LL
w fx
d a. W
(SWHO) 33NVlSIS3a
a, > L
3 S 0 .- c e
Z \ ln W
B z 0
LL
p!
e 3
a,
a, I- S Y ln
c
e .-
12
(SWHO) 33NVlSIS38
13
W ez 2 d 4 W
YI I-
o) > L
3
0 c3 00 a
2
e 2
o)
o) t-
4-
F o) - 4- c 0 m
U 50
Figure 8. Aft Helium Bottle Temperature (S/N 44878) Calibration Curve b
14
100 150 200
TEMPERATURE (OF)
250 300
(SWHO) 33NVlSIS38
h
Y
Q) > L
3 t 0 .- c e * V - 0
h
9 OI
3 Z \ v) Y
9
e 3 c
9)
9) I-
E" 9)
0 m
- c c
L
15
150n 2 3
Commutator Cali brat ion
160
140
120
100
80
60
40
20
0 200 400. 600
TEMPERATURE ( O F )
800 1000
Figure 10. Fin Cuff Temperature (S/N 48792) Calibration Curve
16
1 60
140
1 20
100
80
60
40
20
Hi-Temp Amplifier #1 '
RF Link-- SST II, 231.4MCS
0 200 . 400 600
TEMPERATURE ( O F )
800 lo00
Fiaure 1 1 . Tail Can Bulkhead Temperature (S/N 48794) Calibration Curve Y
17
n 9 c
L
c 0 0
0
18
P) L 6
P) c c 0 m E 5)
P) I
.- e
c L .- Y ul
72 0 r 0
LL
19
h
LL
S 0
A
Z \ wl
a, W
L
4- 2 0 L a,
a, t-
c C 0 - 0 0 V
20
i L 0 >
6
5
4
3
2
1
tttlt t t tttmtttt+i+mmty
0 50 100 150 200 250 300 350 400 450 500 550 600 PRESSURE. ( P S I )
Figure 16. Gas Regulator Pressure (S/N 11081) Calibration Curve
22
0 50 100 150 200 250 300 350 400 450 500 550 600
PRESSURE (PSI )
Figure 18. Fuel Gas Line Pressure (S/N 11081) Calibration Curve
24
I- 3 0
W
(3 4 5 0 > 3 t- z 3 0
2
1
0
I
I
I 50 100 150 200 250 300 350 400 450 500 550 600
PRESSURE (PSI )
Figure 19. Fuel tine Pressure (S/N 11474) Calibration Curve
25
G > t-
i? 5 0
6
5
4
3
2
1
0 50 100 150 200 250 300 350 400 450 500 550 600
PRESSURE (PSI )
Figure 20. Oxidizer Line Pressure (S/N 11086) Calibration Curve
26
0
PRESSURE ( PSI )
Figure 21. Oxidizer Injector Pressure (S/N 11090) Calibration Curve
27
PRESSURE (PSI )
Figure 22. Fuel Injector Pressure (S/N 11093) Calibration Curve
I-
28
W 0 U
> t-
6
PRESSURE (PSI )
Figure 23. Fuel Coolant Inlet Pressure (S/N 11094) Calibration Curve
29
0 50 100 150 200 250 300 350 400 450 500 550 600
PRESSURE (PSI )
Figure 24. Fuel Coolant Outlet Pressure (S/N 11089) Calibration Curve
30
PRESSURE (PSI )
Figure 25. Chamber Pressure (S/N 11088) Calibration Curve
31
C 0 .- .I-
2 n
L
4- al
0 m i;
FIELD (IN MILLIGAUSS)
Figure 27. Lateral Magnetometer (S/N 401) Calibration Curve
33
Lu 0 P 6 > t- i? 5 0
5
4
3
2
1
0 -600 -500 -400 -300 -200 -100 0 +lo0 +200 +300 +40O +600
FIELD (IN MILLIGAUSS)
Figure 28. Longitudinal Magnetometer (S/N 404) Calibration Curve
34
.
/-"A'' EYE
--
- 6 3 5 O I + 6 3 . 5 O
Figure 31. Solar Aspect Sensor, Model 133E Code Reference Diagram
37
- 6 3 . 5 O I + 6 3 . 5 O
Figure 32. Solar Aspect Sensor, Model 133 F Code Reference Diagram
38
cy u) I
i aUOM A0 a N 3 '-1
c
! f r 0
5
I
0 0 0 0 0
t t ? ; t t z z z z z w w w w w
I I I I I t' w n -
39
+ PITCH L TOWARD FIN I
+ YAW L TOWARD FIN II
Figure 34. Transducer Orientation
40
Table 6. Code Table For Adcole Solar Aspect Sensors Models 133 E & F
(Sheet 1 of 6) 0000000 ................ +63.5O 0000001 ................ +62.5' 0000010 ................ +60.5O 0000011 ................ +61.5O 0000100 ................ +56.5' 0~00101 ................ +57.5O 0000110 ................ +59.5" 0000111 ................ +58.5O 0001000 ................ +48.5 0001001 ................ +49.5O 0001010 ................ +51.5 0001011 ................ +50.5 0001100 ................ +55.5 . 0001101 ................ +54.5 . OOOPllO ................ +52.5
0001111 ................ +53.5 . 0010000 ................ +32.5' 0010001 ................ +33.5 O
0010010 ................ +35.5 O
0010011 ................ +34.5 O
0010100 ................ +39.5 O
OOlOPOl ................ +38.5 . 0010110 ................ +36.5 0010111 ................ +37.5 O
41
Table 6 . Code Table For Adcole S o l a r Aspect Sensors Models 133 E & F r'
(Shee t 2 of 6) 001P000 ................ +47.5O
0011001 ................ +46.5O
0011010 ................ +44.5O
001lOl l ................ +45.5O
0011100 ................ +40.5'
0011101 ................ +41.5"
O O l l P l O ................ +43.5"
O O P l P l P ................ +42.5'
OBOOOOO ................ +0.5 .
0100001 ................ +1.50
0100010 ................ +3.50
O l O O O P l ................ +2.5.
ol'oo1oo ................ +7.50
O l O O P O l ................ i-6.5'
OQOOQlO ................ +4.50 0100111 ................ +5 .5"
0101000 ................ +15.5'
O l O l O O f ................ 4-14.5O
0101010 ................ +12.5.
OlO101l ................ +13.5O
O l O P l O O ................ +8.5"
O l O 1 1 O l ................ 4-9.5"
OlOl110 ................ +11.5O
O l O l P P l ................ + 1 0 . 5 O
42
' Table 6 . Code Table For Adcole Solar Aspect Sensors Models 133 E & F (Sheet 3 of 6) 0110000 ................ +31.5 0
0110001 ................ +29.5O OlPOOlO ................ +27.5' 0110011 ................ +28.5' 0110100 ................ +24.5" 0 ~ 1 0 1 0 ~ ................ +25.5. 0110110 ................ +26.5' 0110111 ................ +25.5' OPllOOO ................ +16.5" 0111001 ................ +17.5. 0 ~ ~ ~ 0 ~ 0 ................ +19.5. 0111011 ................ +18.5' 0111100 ................ +23.5" 0111101 ................ +22.5O OlflllO ................ +20.5' OlPllll ................ +21.5' 1000000 ................ -63.5' 1000001 ................ -62.5' 1OO0010 ................ -60.5" 1OOOO11 ................ -61.5' 1000100 ................ -56.5" 1OOOlOl ................ -57.5' 1000110 ................ -59.5O PO00111 ................. -58.5' POOfOOO ................ -48.5'
43
Table 6. Code Table For Adcole S o l a r Aspect Sensors Models 133 E & F (Sheet 4 of 6)
P O O l O O ~ ................ -49.5O 1OOPOPO ................ -51.5" P O O l O P P ................ -50.5" 9001100 ................ -55.5" 1001101 ................ -54.5" l O 0 1 1 P O ................ -52.5" 1001111 ................ -53.5" 1010000 ................ -32.5 O
1010001 ................ -33.5" 1OlOOlO ................ -35.5" 1010011 ................ -34.5 O
1010P00 ................ -39.5 O
1010101 ................ -38.5' 1010110 ................ -36.5 O
loPola1 ................ -37.5 O
1OP1000 ................ -47.5 " 1010001. ................ -46.5 " 1011010 ................ -44.5 O
1011011 ................ -45.5 O
1011POO ................ -40.5" 101llOl ................ -41.5 O lOPP1lO ................ -43.5 " 1011111. ................ -42.5' 1100000 ................ -0.5"
44
a
Table 6 . Code Table For Adcole So lar Aspect Sensors Models 133 E & F
1100001 ................ -1.5 " 1100010 ................ -3.5" 1100011 ................ -2.5" 1100100 ................ -7.5" 1100101 ................ -6.5"' 1100110 ................ -4.5" llOOP1l ................ -5.5" PI01000 ................ -15.5" 1101001 ................ -14.5O 11OPOlO ................ -12.5 " 1101011 ................ -13.5" 1101100 ................ -8.5" 1101101 ................ -9.5" 1101110 ................ -11.5" 1101111 ................ -10.5O 1110000 ................ -31.5" 1110001 ................ -30.5" I110010 ................ -28.5' I110011 ................ -29.5' 111OIOO ................ -24.5" 111O101 ................ -25.5' 1110110 ................ -27.5' 1110111 ................ -26.5" IPIIOOO ................ -16.5"
45
(Sheet 5 of 6)
Code Table For Adcole S o l a r Aspect Sensors Models 133 E & F
(Sheet 6 of 6 )
1 Table 6.
lllP001 ................ -17.5O PlllOlO ................ -19.5" 1lllOlP -18.5O
lllll00 ................ -23.5'
I ................
lllPl0l ................ -22.5O 1111110 ................ -20 .5"
1111111 ................ -21.5O
NOTE :
Extreme r igh t -hand d i g i t i s Most S i g n i f i c a n t D i g i t (MSD) Extreme l e f t -hand d i g i t is Least S i g n i f i c a n t D i g i t (LSD)
46
.
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