MCC-H
0434
CDT
—
236:00
(mil)
t
(Xllll)
:10
"(11101)
(Xllll)
:20
—
236:30
:40
—
:
50
—
237:00
FLIGHT
PLAN
EXIT
G&N
PTC
USING
SM8AYJETCbNFKi
P52
IMU
REALIGN
OPT
3
REFSMMAT
PTC
ORIENTATION
REPORT:
GYRO
TORQUING
ANGLES
CYCLE
CMC
MODE
-
FREE/AUTO
V48
(moi)(xini)
V67
(+99000)(+00020)(+00003)
V49
MNVR
TO
OPTICS
CALIBRATION
ATT
(066,152,350)
HGA
P
^70,
Y
295
P23
CALIBRATION
STAR
N70
(00020)
POO
*
V49
MNVR
TO
SIGHTING
ATT
(084,120,330)
HGA
P
-57,
Y
360
P23
CISLUNAR
NAVIGATION
3
MARKS
ON
EACH
STAR
DURING
TEC,
P23'S
WILL
BE
PER¬
FORMED
ON
A
NON-INTERFERENCE
BASIS
WITH
OTHER
CREW
ACTIVITIES
AS
IF
A
"NO-COMM"
CONTINGENCY
EXISTED.
MCC-H
WILL
UPLINK
A
STATE
VECTOR
WHICH
WILL
BE
STORED
IN
THE
LM
SLOTS.
MCC-H
WILL
COM¬
PUTE
AND
BIAS
MID-COURSE
COR¬
RECTION
MANEUVERS
USING
THE
CSM
VECTOR
UPDATED
BY
P23
DATA.
NOTES
N
GR
AP*
MS
2.
N70
(00000)
(00000)
(00120)
N88
(+15707)(+98142)(+11018)
y
N70
(00000)
(00000)
(00110)
N88
(-38535)(+79355)(+47094)
P52
N71:
N05:
IMU
REALIGN
37
*3
5
OCX?#
2-
N93:
X
_
_
Y
—
.<??/_
z
*lZ
Z*Z_
GET
2
j£
:
if
3*
3.
N70
(00013)
(00000)
(00120)
LOAD
W-MATRIX
EARTH
DISTANCE
~
181,215
NM
57
BELLA
TRIX
(EFH)
50
POLLUX
(ENH)
13
CAPELLA
(EFH)
MISSION
EDITION
DATE
TIME
DAY/REV
PAGE
APOLLO
15
FINAL
(7/26)
7/12/71
236:00
-
237:00
10/TEC
3-348
CHANGE
B
FLIGHT
PLANNING
BRANCH
*
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