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.p136 [[ https://history.nasa.gov/diagrams/ad003.gif | SLA (spacecraft LM adapter) panel]], 4 panels per mission, as many as 36 in heliocentric orbit. 6.6 meter diameter S-IVB (third) stage to 3.9 meter diameter service module. . |
.p136 [[ https://history.nasa.gov/diagrams/ad003.gif | SLA (spacecraft LM adapter) panel]], 4 panels per mission, as many as 36 in heliocentric orbit. 6.6 meter diameter S-IVB (third) stage to 3.9 meter diameter service module. Estimated ( 6.6 x 4.3 to 2.8 ) meters. .p138 '''COAS''' Crewman Optical Alignment Sight, aligned to target on LM .p139 [[ https://history.nasa.gov/ap10fj/pics/docking-config.jpg | probe and drogue docking mechanism ]] .p149 "asteroid" J002E3 probably the S-IVB from Apollo 12 .p157 Unified S-Band, combination of all signals into one 2.1064 GHz (CSM) or 2.1018 GHz (LM) uplink carrier, used for distance and speed doppler. Transponder multiplied frequency by 240/221 for downlink. .p160 Sextant telescope on opposite side of CM main hatch, 0.01 degree precision .p161 SLOS = Star Line Of Sight. .p163 Jim Lovell made P23 measurements and calculated state with P21 to within 500 meters of ground/doppler calculations .p166 |
How Apollo Flew to the Moon
W. David Woods, Praxis 2011, second edition ISBN 978-1-4419-7178-4, Central 629.454 w868h 2011
A useful reference, which I cannot afford to add to my groaning library. Borrowed January 2017
Notes:
- p118 ARIA: Apollo Range Instrumentation Aircraft, EC-135 (like Boeing 707) that relayed voice and recording telemetry.
- p127 PAD: pre-advisory data, spoken numbers uplinked to astronauts to a small form, used for navigation and manual operation in the event of automatic equipment failure
- p130 passing through van Allen belt at "10 km/s": minutes through the inner belt protons, 1.5 hours through the outer belt electrons. In lunar orbital plane, not through the densest equatorial portions of the belts.
p133 EMS Entry Monitor System
p134 TD&E Transposition, docking, and extraction of LM
p136 SLA (spacecraft LM adapter) panel, 4 panels per mission, as many as 36 in heliocentric orbit. 6.6 meter diameter S-IVB (third) stage to 3.9 meter diameter service module. Estimated ( 6.6 x 4.3 to 2.8 ) meters.
p138 COAS Crewman Optical Alignment Sight, aligned to target on LM
p149 "asteroid" J002E3 probably the S-IVB from Apollo 12
- p157 Unified S-Band, combination of all signals into one 2.1064 GHz (CSM) or 2.1018 GHz (LM) uplink carrier, used for distance and speed doppler. Transponder multiplied frequency by 240/221 for downlink.
- p160 Sextant telescope on opposite side of CM main hatch, 0.01 degree precision
- p161 SLOS = Star Line Of Sight.
- p163 Jim Lovell made P23 measurements and calculated state with P21 to within 500 meters of ground/doppler calculations
- p166