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.

 

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