Selected Mission Weights (lbs)[1]
|
Apollo 7 |
Apollo 8 |
Apollo 9 |
Apollo 10 |
Apollo 11 |
Apollo 12 |
Apollo 13 |
Apollo 14 |
Apollo 15 |
Apollo 16 |
Apollo 17 |
|
|
|
|
|
|
|
|
|
|
|
|
CSM/LM at EOI |
36,419 |
87,382 |
95,231 |
98,273 |
100,756.4 |
101,126.9 |
101,261.2 |
102,083.6 |
107,142 |
107,226 |
107,161 |
CSM/LM at Separation |
--- |
--- |
--- |
94,063 |
96,566.6 |
--- |
--- |
--- |
--- |
--- |
--- |
CSM/LM at Transposition & Docking |
--- |
--- |
91,055 |
94,243 |
96,767.5 |
97,119.8 |
97,219.4 |
98,037.2 |
103,105 |
103,175 |
103,167 |
CSM at Transposition & Docking |
--- |
--- |
58,925 |
63,560 |
63,473.0 |
63,535.6 |
63,720.3 |
64,388.0 |
66,885 |
66,923 |
66,893 |
LM at Transposition & Docking |
--- |
--- |
32,130 |
30,683 |
33,294.5 |
33,584.2 |
33,499.1 |
33,649.2 |
36,220 |
36,252 |
36,274 |
CSM/LM at 1st MCC Ignition |
--- |
63,307 |
--- |
93,889 |
96,418.2 |
96,870.6 |
97,081.5 |
97,901.5 |
--- |
--- |
--- |
CSM/LM at 1st MCC Cutoff |
--- |
--- |
--- |
93,413 |
96,204.2 |
96,401.2 |
96,851.1 |
--- |
--- |
--- |
--- |
CSM/LM Before Cryogenic Tank Anomaly |
--- |
--- |
--- |
--- |
--- |
--- |
96,646.9 |
--- |
--- |
--- |
--- |
CSM/LM After Cryogenic Tank Anomaly |
--- |
--- |
--- |
--- |
--- |
--- |
96,038.7 |
--- |
--- |
--- |
--- |
CSM/LM at 2nd MCC Ignition |
--- |
62,845 |
--- |
--- |
--- |
--- |
95,959.9 |
97,104.1 |
--- |
--- |
--- |
CSM/LM at 2nd MCC Cutoff |
--- |
--- |
--- |
--- |
--- |
--- |
95,647.1 |
--- |
--- |
--- |
--- |
CSM at TEI Ignition |
--- |
45,931 |
--- |
37,254 |
36,965.7 |
34,130.6 |
95,424.0 |
34,554.4 |
35,899 |
38,697 |
36,394 |
CSM at TEI Cutoff |
--- |
--- |
--- |
26,172 |
26,792.7 |
25,724.5 |
87,456.0 |
--- |
--- |
--- |
--- |
CSM at 3rd MCC Ignition |
--- |
32,008 |
--- |
--- |
--- |
--- |
87,325.3 |
24,631.9 |
--- |
--- |
--- |
CSM at 3rd MCC Cutoff |
--- |
--- |
--- |
--- |
--- |
--- |
87,263.3 |
--- |
--- |
--- |
--- |
CSM/LM at LOI Ignition |
--- |
62,827 |
--- |
93,319 |
96,061.6 |
96,261.1 |
--- |
97,033.1 |
102,589 |
102,642 |
102,639 |
CSM/LM at LOI Cutoff |
--- |
46,743 |
--- |
69,429 |
72,037.6 |
72,335.6 |
--- |
71,823.0 |
76,329 |
77,647 |
76,540 |
CSM/LM at Circularization Ignition |
--- |
46,716 |
--- |
69,385 |
72,019.9 |
72,243.7 |
--- |
--- |
--- |
--- |
--- |
CSM/LM at Circularization Cutoff |
--- |
--- |
--- |
68,455 |
70,905.9 |
71,028.4 |
--- |
--- |
--- |
--- |
--- |
CSM/LM at Descent Orbit Insertion |
--- |
--- |
--- |
--- |
--- |
--- |
--- |
71,768.8 |
76,278 |
77,595 |
76,354 |
CSM/LM at Separation for Lunar Landing |
--- |
--- |
--- |
68,238 |
70,760.3 |
70,897.3 |
--- |
70,162.3 |
74,460 |
76,590 |
74,762 |
CSM at Separation for Lunar Landing |
--- |
--- |
--- |
37,072 |
37,076.8 |
36,911.8 |
--- |
36,036.4 |
37,742 |
39,847 |
37,991 |
LM at Separation for Lunar Landing |
--- |
--- |
--- |
31,166 |
33,683.5 |
33,985.5 |
--- |
34,125.9 |
36,718 |
36,743 |
36,771 |
LM at Powered Descent Initiation |
--- |
--- |
--- |
--- |
--- |
--- |
--- |
34,067.8 |
36,634 |
36,617 |
36,686 |
LM at Descent Orbit Insertion Ignition |
--- |
--- |
--- |
31,137 |
33,669.6 |
33,971.8 |
--- |
--- |
--- |
--- |
--- |
LM at Descent Orbit Insertion Cutoff |
--- |
--- |
--- |
30,903 |
33,401.6 |
33,719.3 |
--- |
--- |
--- |
--- |
--- |
LM at Lunar Landing |
--- |
--- |
--- |
--- |
16,153.2 |
16,564.2 |
--- |
16,371.7 |
18,175 |
18,208 |
18,305 |
CSM at Plane Burn Time |
--- |
--- |
--- |
--- |
--- |
--- |
--- |
35,610.4 |
37,219 |
38,994 |
37,464 |
CSM at Circularization Ignition |
--- |
--- |
--- |
--- |
--- |
--- |
--- |
35,996.3 |
37,716 |
39,595 |
37,960 |
LM at Phasing Ignition |
--- |
--- |
--- |
30,824 |
--- |
--- |
--- |
--- |
--- |
--- |
--- |
LM at Phasing Cutoff |
--- |
--- |
--- |
30,283 |
--- |
--- |
--- |
--- |
--- |
--- |
--- |
LM at Fuel Depletion |
--- |
--- |
5,616 |
5,243 |
--- |
--- |
--- |
--- |
--- |
--- |
--- |
CSM/LM Ascent Stage at Docking |
--- |
--- |
36,828 |
44,930 |
42,585.4 |
41,071.8 |
--- |
39,906.8 |
41,754 |
44,318 |
41,914 |
CSM at Docking |
--- |
--- |
26,895 |
36,995 |
36,847.4 |
35,306.2 |
--- |
34,125.5 |
35,928 |
38,452 |
36,036 |
LM Ascent Stage at Lunar Liftoff |
--- |
--- |
--- |
--- |
10,776.6 |
10,749.6 |
--- |
10,779.8 |
10,915 |
10,949 |
10,997 |
LM Ascent Stage at Orbit Insertion for Docking |
--- |
--- |
--- |
8,077 |
5,928.6 |
5,965.6 |
--- |
5,917.8 |
5,985 |
6,001 |
6,042 |
LM Ascent Stage at Terminal Phase Initiation |
--- |
--- |
--- |
--- |
--- |
--- |
--- |
5,880.1 |
5,965 |
5,972 |
5,970 |
LM Ascent Stage After Staging |
--- |
--- |
--- |
8,273 |
--- |
--- |
--- |
--- |
--- |
--- |
--- |
LM Ascent Stage at Coelliptic Sequence Initiation |
--- |
--- |
--- |
8,052 |
5,881.5 |
5,885.9 |
--- |
--- |
--- |
--- |
--- |
LM Ascent Stage at Docking |
--- |
--- |
9,933 |
7,935 |
5,738.0 |
5,765.6 |
--- |
5,781.3 |
5,826 |
5,866 |
5,878 |
CSM at After Post-Docking Jettison |
--- |
--- |
27,139 |
--- |
37,100.5 |
35,622.9 |
--- |
34,596.3 |
36,407 |
38,992 |
36,619 |
LM Ascent Stage After Post-Docking Jettison |
--- |
--- |
--- |
7,663 |
5,462.5 |
5,436.5 |
--- |
5,307.6 |
5,325 |
5,306 |
5,277 |
CSM (CSM/LM) at Subsatellite Jettison |
--- |
--- |
--- |
--- |
--- |
--- |
--- |
--- |
36,019 |
38,830 |
--- |
CSM at 4th MCC Ignition |
--- |
--- |
--- |
--- |
--- |
--- |
87,132.1 |
--- |
--- |
--- |
--- |
CSM at 4th MCC Cutoff |
--- |
--- |
--- |
--- |
--- |
--- |
87,101.5 |
--- |
--- |
--- |
--- |
CSM at Pre-Entry Separation |
23,435 |
31,768 |
24,183 |
25,095 |
26,656.5 |
25,444.2 |
--- |
24,375.0 |
26,323 |
27,225 |
26,659 |
CSM/LM Before CSM/LM Separation |
--- |
--- |
--- |
--- |
--- |
--- |
87,057.3 |
--- |
--- |
--- |
--- |
CM/LM After CSM/LM Separation |
--- |
--- |
--- |
--- |
--- |
--- |
37,109.7 |
--- |
--- |
--- |
--- |
SM After Pre-Entry Separation |
11,071 |
19,589 |
11,924 |
12,957 |
14,549.1 |
13,160.7 |
--- |
11,659.9 |
13,358 |
14,199 |
13,507 |
CM After Pre-Entry Separation |
12,364 |
12,179 |
12,259 |
12,138 |
12,107.4 |
12,283.5 |
12,367.6 |
12,715.1 |
12,965 |
13,026 |
13,152 |
CM at Entry |
12,356 |
12,171 |
12,257 |
12,137 |
12,095.5 |
12,275.5 |
12,361.4 |
12,703.5 |
12,953 |
13,015 |
13,140 |
CM at Drogue Deployment |
11,936 |
11,712 |
11,839 |
11,639 |
11,603.7 |
11,785.7 |
11,869.4 |
--- |
--- |
--- |
--- |
CM at Main Parachute Deployment |
11,855 |
11,631 |
11,758 |
11,558 |
11,318.9 |
11,496.1 |
11,579.8 |
12,130.8 |
12,381 |
12,442 |
12,567 |
CM at Landing |
11,409 |
10,977 |
11,094 |
10,901 |
10,873.0 |
11,050.2 |
11,132.9 |
11,481.2 |
11,731 |
11,995 |
12,120 |
[1]Compiled from mission reports. Apollo 7 and Apollo 8 did not have a LM. Apollo 13 includes CSM and LM until separation before Earth entry.