Launch Vehicle/Spacecraft Key Facts

	Apollo 7	Apollo 8	Apollo 9	Apollo 10	Apollo 11	Apollo 12	Apollo 13	Apollo 14	Apollo 15	Apollo 16	Apollo 17
LM Descent Stage	---	---
Diameter, ft	---	---	14.083	14.083	14.083	14.083	14.083	14.083	14.083	14.083	14.083
Height, ft	---	---	10.583	10.583	10.583	10.583	10.583	10.583	10.583	10.583	10.583
Weight, dry, lb	---	---	4,265	4,703	4,483	4,875	4,650	4,716	6,179	6,083	6,155
Maximum rated thrust, lb	---	---	9,870	9,870	9,870	9,870	9,870	9,870	9,870	9,870	9,870
LM Ascent Stage	---	---
Diameter, ft	---	---	14.083	14.083	14.083	14.083	14.083	14.083	14.083	14.083	14.083
Height, ft	---	---	12.333	12.333	12.333	12.333	12.333	12.333	12.333	12.333	12.333
Cabin volume, cu ft	---	---	235	235	235	235	235	235	235	235	235
Habitable volume, cu ft	---	---	160	160	160	160	160	160	160	160	160
Crew compartment height, ft	---	---	7.667	7.667	7.667	7.667	7.667	7.667	7.833	7.833	7.833
Crew compartment depth, ft	---	---	3.500	3.500	3.500	3.500	3.500	3.500	3.500	3.500	3.500
Weight, dry, lb	---	---	5,071	4,781	4,804	4,760	4,668	4,691	4,690	4,704	4,729
Maximum rated thrust, lb	---	---	2,524	1,650	3,218	3,224	N/A	3,218.2	3,225.6	3,224.7	3,234.8
Lunar Rover Vehicle (LRV)
Contractor	---	---	---	---	---	---	---	---	Boeing	Boeing	Boeing
Length, ft	---	---	---	---	---	---	---	---	10.167	10.167	10.167
Width, ft	---	---	---	---	---	---	---	---	6.000	6.000	6.000
Wheel base, ft	---	---	---	---	---	---	---	---	7.500	7.500	7.500
Weight, lb	---	---	---	---	---	---	---	---	462	462	462
Payload capacity, lb	---	---	---	---	---	---	---	---	1,080	1,080	1,080
Command Module (CM)
Contractor	North American Rockwell	North American Rockwell	North American Rockwell	North American Rockwell	North American Rockwell	North American Rockwell	North American Rockwell	North American Rockwell	North American Rockwell	North American Rockwell	North American Rockwell
Diameter, ft	12.833	12.833	12.833	12.833	12.833	12.833	12.833	12.833	12.833	12.833	12.833
Height, ft	11.417	11.417	11.417	11.417	11.417	11.417	11.417	11.417	11.417	11.417	11.417
Docking probe cone, ft	2.583	2.583	2.583	2.583	2.583	2.583	2.583	2.583	2.583	2.583	2.583
Main structure, ft	6.750	6.750	6.750	6.750	6.750	6.750	6.750	6.750	6.750	6.750	6.750
Aft/heat shield, ft	2.083	2.083	2.083	2.083	2.083	2.083	2.083	2.083	2.083	2.083	2.083
Weight, lb	12,659	12,392	12,405	12,277	12,250	12,365	12,365	12,831	12,831	12,874	12,874
Habitable volume, cu ft	210	210	210	210	210	210	210	210	210	210	210
Launch Escape System (LES)
Contractor	North American Rockwell	North American Rockwell	North American Rockwell	North American Rockwell	North American Rockwell	North American Rockwell	North American Rockwell	North American Rockwell	North American Rockwell	North American Rockwell	North American Rockwell
Diameter, ft	4.000	4.000	4.000	4.000	4.000	4.000	4.000	4.000	4.000	4.000	4.000
Height, ft	33.460	33.460	33.460	33.460	33.460	33.460	33.460	33.460	33.460	33.460	33.460
Rocket motors (1 each)
Thrust, LES, lb	155,000	147,000	147,000	147,000	147,000	147,000	147,000	147,000	147,000	147,000	147,000
Thrust, pitch control motor, lb	3,000	2,400	2,400	2,400	2,400	2,400	2,400	2,400	2,400	2,400	2,400
Thrust tower jettison motor, lb	33,000	31,500	31,500	31,500	31,500	31,500	31,500	31,500	31,500	31,500	31,500
Total Vehicle Height (ft)	223.488	363.013	363.013	363.013	363.013	363.013	363.013	363.013	363.013	363.013	363.013

LM ascent and descent stages, LRV and CM dry weights are as published in mission press kits. All other weights are “as flown.”

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