DATE
6/l_4/7i
2-17
1
Verify
CSM
In
Min
DEADBAND
ATT
HOLD
2
Calculate
LM
Gimbal
Angles
=Rc
(1-1)
+
=CM
OG
300.00
n
180.00
MG
360.00
LM
(ooo!oo)
(300.00)
+
/o
3.3*7
(105.50)
(359.90)
2£/
&
3?y.
63
(285.50)
(000.10)
3
V41
N20E
COARSE
ALIGN
IMU
F
21
22
LOAD
ICDU
ANGLE
OG,IG,MG
(.01°)
(NO
ATT
LT
-
ON,
FDAI
Torques)
FDAI
ANGLES
000,286,060
4
V40
N20E
ZERO
CDU
(NO
ATT
Lt-Off)
RCS
C/0
RR
SELF
TEST
DROGUE
&
PROBE
98:50
ASCENT/LUNAR
BAT
CHECKOUT
CB
(16)
EPS:
ASC
ECA
CONT
-
CLOSE
POWER/TEMP
MON
SEL-LUN
LMP
LUNAR
BAT
OFF/RESET;
tb
-
b/p,
then
ON;
tb
-
LMP
(VERIFY
LUNAR
BAT
CURRENT)
LMP
LUNAR
BAT
-
OFF/RESET;
tb
-
b/p
POWER
TEMP
MON
SEL-BAT
5
BAT
5
NORMAL
LMP
FEED
-
ON;
tb
-
gray
(VERIFY
BAT
5
CURRENT)
LMP
BAT
1
HI
V
-
OFF/RESET;
tb
-
b/p
CDR
LUNAR
BAT
OFF/RESET;
tb
-
b/p,
then
ON;
tb
-
CDR
(VERIFY
LUNAR
BAT
CURRENT)
CDR
LUNAR
BAT
-
OFF/RESET;
tb
-
b/p
POWER
TEMP
MON
SEL
-
BAT
6
BAT
6
NORMAL
CDR
FEED
-
ON;
tb
-
gray
(VERIFY
BAT
6
CURRENT)
CDR
BAT
4
HI
V
-
OFF/RESET;
tb
-
b/p
POWER/TEMP
MON
SEL
-
CDR
BUS,
LMP
BUS
IMU
C/A
BAT
C/0
P52
ALIGN
RCS
PRESS
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