From 173e6152080b9821c278102b8b038501191fc564 Mon Sep 17 00:00:00 2001 From: Nathan Scott Date: Mon, 19 Oct 2020 17:11:22 +1100 Subject: [PATCH] Page 618 MIME-Version: 1.0 Content-Type: text/plain; charset=UTF-8 Content-Transfer-Encoding: 8bit http://www.ibiblio.org/apollo/ScansForConversion/Luminary099/0618.jpg R0011 (L32) remove extra hyphen R0014 (L37) remove word "TIME" not in scan R0015 (L38) remove extra hyphen R0021 (L46) (un)correct typo in scan: "FLIGHT" → "FLIGNT" R0043 (L79) remove comma not in scan Comment out empty lines within comment blocks, for consistency --- Luminary099/P32-P35_P72-P75.agc | 32 ++++++++++++++++---------------- 1 file changed, 16 insertions(+), 16 deletions(-) diff --git a/Luminary099/P32-P35_P72-P75.agc b/Luminary099/P32-P35_P72-P75.agc index c2435e8..d6a6626 100644 --- a/Luminary099/P32-P35_P72-P75.agc +++ b/Luminary099/P32-P35_P72-P75.agc @@ -29,54 +29,54 @@ # Page 618 # COELLIPTIC SEQUENCE INITIATION (CSI) PROGRAMS (P32 AND P72) # -# MOD NO -1 LOG SECTION -- P32-P35, P72-P75 +# MOD NO -1 LOG SECTION - P32-P35, P72-P75 # MOD BY WHITE.P DATE 1JUNE67 # # PURPOSE - -# (1) TO CALCULATE PARAMETERS ASSOCIATED WITH THE TIME FOLLOWING -# CONCENTRIC FLIGHT PLAN MANEUVERS -- THE CO-ELLIPTIC SEQUENCE +# +# (1) TO CALCULATE PARAMETERS ASSOCIATED WITH THE FOLLOWING +# CONCENTRIC FLIGHT PLAN MANEUVERS - THE CO-ELLIPTIC SEQUENCE # INITIATION (CSI) MANEUVER AND THE CONSTANT DELTA ALTITUDE # (CDH) MANEUVER. - +# # (2) TO CALCULATE THESE PARAMETERS BASED UPON MANEUVER DATA # APPROVED AND KEYED INTO THE DSKY BY THE ASTRONAUT. - +# # (3) TO DISPLAY TO THE ASTRONAUT AND THE GROUND DEPENDENT VARIABLES -# ASSOCIATED WITH THE CONCENTRIC FLIGHT PLAN MANEUVERS FOR +# ASSOCIATED WITH THE CONCENTRIC FLIGNT PLAN MANEUVERS FOR # APPROVAL BY THE ASTRONAUT/GROUND. - +# # (4) TO STORE THE CSI TARGET PARAMETERS FOR USE BY THE DESIRED # THRUSTING PROGRAM. # # ASSUMPTIONS - +# # (1) AT A SELECTED TPI TIME THE LINE OF SIGHT BETWEEN THE ACTIVE # AND PASSIVE VEHICLES IS SELECTED TO BE A PRESCRIBED ANGLE (E) # FROM THE HORIZONTAL PLANE DEFINED BY THE ACTIVE VEHICLE # POSITION. - +# # (2) THE TIME BETWEEN CSI IGNITION AND CDH IGNITION MUST BE # COMPUTED TO BE GREATER THAN 10 MINUTES FOR SUCCESSFUL # COMPLETION OF THE PROGRAM. - +# # (3) THE TIME BETWEEN CDH IGNITION AND TPI IGNITION MUST BE # COMPUTED TO BE GREATER THAN 10 MINUTES FOR SUCCESSFUL # COMPLETION OF THE PROGRAM. - +# # (4) CDH DELTA V IS SELECTED TO MINIMIZE THE VARIATION OF THE # ALTITUDE DIFFERENCE BETWEEN THE ORBITS. - +# # (5) CSI BURN IS DEFINED SUCH THAT THE IMPULSIVE DELTA V IS IN THE # HORIZONTAL PLANE DEFINED BY THE ACTIVE VEHICLE POSITION AT CSI # IGNITION. - +# # (6) THE PERICENTER ALTITUDE OF THE ORBIT FOLLOWING CSI AND CDH # MUST BE GREATER THAN 35,000 FT (LUNAR ORBIT) OR 85 NM (EARTH # ORBIT) FOR SUCCESSFUL COMPLETION OF THIS PROGRAM. - +# # (7) THE CSI AND CDH MANEUVERS ARE ORIGINALLY ASSUMED TO BE -# PARALLEL TO THE PLANE OF THE CSM ORBIT. HOWEVER, CREW +# PARALLEL TO THE PLANE OF THE CSM ORBIT. HOWEVER CREW # Page 619 # MODIFICATION OF DELTA V (LV) COMPONENTS MAY RESULT IN AN # OUT-OF-PLANE CSI MANEUVER