From ad36f094e9508533f070112d0c51e2d9510df60b Mon Sep 17 00:00:00 2001 From: Nathan Scott Date: Sat, 24 Oct 2020 23:12:50 +1100 Subject: [PATCH] Page 624 MIME-Version: 1.0 Content-Type: text/plain; charset=UTF-8 Content-Transfer-Encoding: 8bit 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 --- Luminary099/P32-P35_P72-P75.agc | 11 ++++++----- 1 file changed, 6 insertions(+), 5 deletions(-) diff --git a/Luminary099/P32-P35_P72-P75.agc b/Luminary099/P32-P35_P72-P75.agc index 3bba50a..8e36ba7 100644 --- a/Luminary099/P32-P35_P72-P75.agc +++ b/Luminary099/P32-P35_P72-P75.agc @@ -322,9 +322,9 @@ P32/P72F STORE T2TOT3 # Page 624 # 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 # # (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 # CO-ELLIPTIC SEQUENCE INITIATION (CSI) PROGRAM (P32/P72). -# THEREFORE -- +# THERFORE - # # (A) AT A SELECTED TPI TIME (NOW IN STORAGE) THE LINE OF SIGHT # 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. # # (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 # IN THE HORIZONTAL PLANE DEFINED BY ACTIVE VEHICLE +# # 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 # ORBIT OR 85 NM FOR EARTH ORBIT. #