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 . [[ http://history.nasa.gov/ap10fj/pdf/19730064165_a10mr-supp10-entry-postflight-analysis.pdf | Entry Postflight Analysis ]]
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== Apollo 11 ==
 . [[ https://www.hq.nasa.gov/alsj/a11/A11_MissionReport.pdf | Mission report ]]
 . page 7-12 120/359 TABLE 7-VI I . - ENTRY TRAJECTORY PARAMETERS
 . Entry at 400 kft (122 km) at 195:03:05.7
 . [[ https://history.nasa.gov/ap11fj/pdf/19740072963_as11-entry-analysis-19700220.pdf | Entry Postflight Analysis ]]
   . 1st maximum load factor 6.73g 31,810ft/s
   . 1st minimum load factor 0.48g 20,500ft/s
   . 2nd maximum load factor 6.00g 12,390ft/s
  . Table III
||EI time|| Load g|| V f/s ||range n mi|| ° Bank ||Rdot f/s||
|| 0:00 || 0.000 || 36190 || 1593 || || ||
|| 0:28 || 0.049 || 36276 || 1418 || || ||
|| 0:30 || || 36277 || || 0.0 || -3186 ||
|| 1:18 || || || || || -666 ||
|| 1:30 || || 30176 || || 54.43 || 211 ||
|| 1:56 || 1.057 || 22091 || || -86.68 || ||
{{attachment:a11LD.png}}
{{attachment:a11RDOT.png}}
{{attachment:a11alt.png}}
{{attachment:a11ems.png}}
{{attachment:a11gee.png}}
{{attachment:a11range.png}}
{{attachment:a11roll.png}}
{{attachment:a11vel.png}}
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== Apollo 12 ==
 . [[ https://www.hq.nasa.gov/alsj/a12/A12_MissionReport.pdf | Mission report ]]
 . page 5-14 98/310 TABLE 5-IX . - ENTRY TRAJECTORY PARAMETERS
 . Entry at 400 kft (122 km) at 244:22:19.1
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== Apollo 13 ==
 . [[ https://www.hq.nasa.gov/alsj/a13/A13_MissionReport.pdf | Mission report ]]
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== Apollo 11 ==
== Apollo 12 ==
== Apollo 13 ==
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 . [[ https://www.hq.nasa.gov/alsj/a14/A14MRntrs.pdf | Mission report ]]
 . page
 . Entry at 400 kft (122 km) at
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 . [[ https://www.hq.nasa.gov/alsj/a15/ap15mr.pdf | Mission report ]]
 . page
 . Entry at 400 kft (122 km) at
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 . [[ https://www.hq.nasa.gov/alsj/a16/A16_MissionReport.pdf | Mission report ]]
 . page
 . Entry at 400 kft (122 km) at
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 . [[ https://www.hq.nasa.gov/alsj/a17/A17_MissionReport.pdf | Mission report ]]
 . page
 . Entry at 400 kft (122 km) at
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Apollo Entry

From Apollo mission reports here

Apollo 7 and 9 were earth orbit, slower reentry. Apollo 8 and 10 through 17 were lunar missions with high speed reentry of the command module. Apollo 11,12, and 14-17 were landing missions.


Apollo 8

  • Mission report

  • page 5-10, 53/252 TABLE 5-V . - ENTRY TRAJECTORY PARAMETERS
  • Entry at 400 kft (122 km) at 146:46:12.8
  • page 6-67 to 6-69 entry graphs

Roll

a8r.png

Entry Monitor System Scroll

a8a.png a8b.png


Apollo 10

  • Mission report

  • page 6-13, 54/323 TABLE 6-VI I . - ENTRY TRAJECTORY PARAMETERS
  • Entry at 400 kft (122 km) at 191:48:54.5

Entry Monitor System Scroll

a10.png


Apollo 11

  • Mission report

  • page 7-12 120/359 TABLE 7-VI I . - ENTRY TRAJECTORY PARAMETERS
  • Entry at 400 kft (122 km) at 195:03:05.7
  • Entry Postflight Analysis

    • 1st maximum load factor 6.73g 31,810ft/s
    • 1st minimum load factor 0.48g 20,500ft/s
    • 2nd maximum load factor 6.00g 12,390ft/s
    • Table III

EI time

Load g

V f/s

range n mi

° Bank

Rdot f/s

0:00

0.000

36190

1593

0:28

0.049

36276

1418

0:30

36277

0.0

-3186

1:18

-666

1:30

30176

54.43

211

1:56

1.057

22091

-86.68

a11LD.png a11RDOT.png a11alt.png a11ems.png a11gee.png a11range.png a11roll.png a11vel.png


Apollo 12

  • Mission report

  • page 5-14 98/310 TABLE 5-IX . - ENTRY TRAJECTORY PARAMETERS
  • Entry at 400 kft (122 km) at 244:22:19.1


Apollo 13


Apollo 14


Apollo 15


Apollo 16


Apollo 17


ApolloEntry (last edited 2017-11-22 23:14:55 by KeithLofstrom)