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https://www.ibiblio.org/apollo/ScansForConversion/Luminary099/0027.jpg

R0956 (L1046) correct `WIL` → `WILL`
Comment out empty lines
Realign whitespace to scan
This commit is contained in:
Nathan Scott 2020-11-01 11:53:21 +11:00
parent 4cbbc9c605
commit b1b742329b
1 changed files with 19 additions and 19 deletions
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38
Luminary099/ASSEMBLY_AND_OPERATION_INFORMATION.agc
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@ -1039,26 +1039,26 @@
# KEY IN DENOTES KEY IN OF DATA THRU THE DSKY
# Page 27
# OPTION CODES FOR LUMINARY
# THE SPECIFIED OPTION CODES WIL BE FLASHED IN COMPONENT R1 IN
# OPTION CODES FOR LUMINARY
#
# THE SPECIFIED OPTION CODES WILL BE FLASHED IN COMPONENT R1 IN
# CONJUNCTION WITH V04N06 OR V04N12 (FOR EXTENDED VERBS) TO REQUEST THE
# ASTRONAUT TO LOAD INTO COMPONENT R2 THE OPTION HE DESIRES.
# *9 *17 *52 *11 *25 COLUMN
#
# *9 *17 *52 *11 *25 COLUMN
#
# OPTION
# CODE PURPOSE INPUT FOR COMPONENT 2 PROGRAM(S) APPLICABILITY
# 00001 SPECIFY IMU ORIENTATION 1=PREF 2=NOM 3=REFSMMAT P52 ALL
# 4=LAND SITE
# 00002 SPECIFY VEHICLE 1=THIS 2=OTHER P21,R30 ALL
# 00003 SPECIFY TRACKING ATTITUDE 1=PREFERRED 2=OTHER R63 ALL
# 00004 SPECIFY RADAR 1=RR 2=LR R04 SUNDANCE + LUMINARY
# 00005 SPECIFY SOR PHASE 1=FIRST 2=SECOND P38 COLOSSUS + LUMINARY
# 00006 SPECIFY RR COARSE ALIGN OPTION 1=LOCKON 2=CONTINUOUS DESIG. V41N72 SUNDANCE + LUMINARY
# 00010 SPECIFY ALIGNMENT MODE 0=ANY TIME 1=REFSMMAT +G P57 LUMINARY
# 2=TWO BODIES 3=ONE BODY + G
# 00012 SPECIFY CSM ORBIT OPTION 1=NO ORBIT CHANGE 2=CHANGE P22 LUMINARY
# ORBIT TO PASS OVER LM
# CODE PURPOSE INPUT FOR COMPONENT 2 PROGRAM(S) APPLICABILITY
#
# 00001 SPECIFY IMU ORIENTATION 1=PREF 2=NOM 3=REFSMMAT P52 ALL
# 4=LAND SITE
# 00002 SPECIFY VEHICLE 1=THIS 2=OTHER P21,R30 ALL
# 00003 SPECIFY TRACKING ATTITUDE 1=PREFERRED 2=OTHER R63 ALL
# 00004 SPECIFY RADAR 1=RR 2=LR R04 SUNDANCE + LUMINARY
# 00005 SPECIFY SOR PHASE 1=FIRST 2=SECOND P38 COLOSSUS + LUMINARY
# 00006 SPECIFY RR COARSE ALIGN OPTION 1=LOCKON 2=CONTINUOUS DESIG. V41N72 SUNDANCE + LUMINARY
# 00010 SPECIFY ALIGNMENT MODE 0=ANY TIME 1=REFSMMAT +G P57 LUMINARY
# 2=TWO BODIES 3=ONE BODY + G
# 00012 SPECIFY CSM ORBIT OPTION 1=NO ORBIT CHANGE 2=CHANGE P22 LUMINARY
# ORBIT TO PASS OVER LM