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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.
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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. 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

  • p139 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

HowApollo (last edited 2017-01-24 16:01:38 by KeithLofstrom)