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Page 624

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https://www.ibiblio.org/apollo/ScansForConversion/Luminary099/0624.jpg

Add missing empty line (L325) after P1010
R1011 (L325) correct "LOC" → "LOG"; remove extra hyphen
R1012 (L325) correct "WHITE, P." → "WHITE.P"; correct "DATE:" → "DATE"; correct "1 JUNE 67" → "1JUNE67"
Remove empty line (L327) not in scan (after R1013)
R1026 (L347) (un)correct "THEREFORE" → "THERFORE"; remove extra hyphen
R1036 (L361) (un)correct "MINIMIZED" → "MINMIZED"
Add missing empty line (L365) after R1038
R1039 (L368) remove space before tab
This commit is contained in:
Nathan Scott 2020-10-24 23:12:50 +11:00
parent 93cf8bb9bd
commit ad36f094e9
1 changed files with 6 additions and 5 deletions
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11
Luminary099/P32-P35_P72-P75.agc
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@ -322,9 +322,9 @@ P32/P72F STORE T2TOT3
# Page 624 # Page 624
# CONSTANT DELTA HEIGHT (CDH) PROGRAMS (P33 AND P73) # CONSTANT DELTA HEIGHT (CDH) PROGRAMS (P33 AND P73)
# MOD NO -1 LOC SECTION -- P32-P35, P72-P75
# MOD BY WHITE, P. DATE: 1 JUNE 67
# #
# MOD NO -1 LOG SECTION - P32-P35, P72-P75
# MOD BY WHITE.P DATE 1JUNE67
# PURPOSE # PURPOSE
# #
# (1) TO CALCULATE PARAMETERS ASSOCIATED WITH THE CONSTANT DELTA # (1) TO CALCULATE PARAMETERS ASSOCIATED WITH THE CONSTANT DELTA
@ -344,7 +344,7 @@ P32/P72F STORE T2TOT3
# #
# (1) THIS PROGRAM IS BASED UPON PREVIOUS COMPLETION OF THE # (1) THIS PROGRAM IS BASED UPON PREVIOUS COMPLETION OF THE
# CO-ELLIPTIC SEQUENCE INITIATION (CSI) PROGRAM (P32/P72). # CO-ELLIPTIC SEQUENCE INITIATION (CSI) PROGRAM (P32/P72).
# THEREFORE -- # THERFORE -
# #
# (A) AT A SELECTED TPI TIME (NOW IN STORAGE) THE LINE OF SIGHT # (A) AT A SELECTED TPI TIME (NOW IN STORAGE) THE LINE OF SIGHT
# BETWEEN THE ACTIVE AND PASSIVE VEHICLES WAS SELECTED TO BE # BETWEEN THE ACTIVE AND PASSIVE VEHICLES WAS SELECTED TO BE
@ -358,13 +358,14 @@ P32/P72F STORE T2TOT3
# COMPUTED TO BE GREATER THAN 10 MINUTES. # COMPUTED TO BE GREATER THAN 10 MINUTES.
# #
# (D) THE VARIATION OF THE ALTITUDE DIFFERENCE BETWEEN THE # (D) THE VARIATION OF THE ALTITUDE DIFFERENCE BETWEEN THE
# ORBITS WAS MINIMIZED. # ORBITS WAS MINMIZED.
# #
# (E) CSI BURN WAS DEFINED SUCH THAT THE IMPULSIVE DELTA V WAS # (E) CSI BURN WAS DEFINED SUCH THAT THE IMPULSIVE DELTA V WAS
# IN THE HORIZONTAL PLANE DEFINED BY ACTIVE VEHICLE # IN THE HORIZONTAL PLANE DEFINED BY ACTIVE VEHICLE
#
# POSITION AT CSI IGNITION. # POSITION AT CSI IGNITION.
# #
# (F) THE PERICENTER ALTITUDES OF THE ORBITS FOLLOWING CSI AND # (F) THE PERICENTER ALTITUDES OF THE ORBITS FOLLOWING CSI AND
# CDH WERE COMPUTED TO BE GREATER THAN 35,000 FT FOR LUNAR # CDH WERE COMPUTED TO BE GREATER THAN 35,000 FT FOR LUNAR
# ORBIT OR 85 NM FOR EARTH ORBIT. # ORBIT OR 85 NM FOR EARTH ORBIT.
# #