COMPILATION OF CA lBRATIO'N7 :FOR AEROBEE FUGH 3'-GP- · 2013-08-31 · FM/FM Telemetry System...

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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

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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)



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


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




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



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




F i n Cuff Temperature (Tfc)

T a i l Can Bulkhead Temperature

Ground (Ttp)



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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