📷 NASA Johnson Space Center / Wikimedia Commons (Public domain)
🚀 Full Specifications
| Designation | CSM |
| Manufacturer | North American Aviation (later North American Rockwell) |
| Operator | NASA |
| Country | 🇺🇸 USA |
| First Launch | 1966 |
| Service Entry | 1968 |
| Retired | 1975 |
| Crew Capacity | 3 |
| Height / Length | 11 m (36.1 ft) |
| Diameter / Span | 3.9 m (12.8 ft) |
| Mass | 30,300 kg (66,812 lb) |
| Engines | 1 × AJ10-137 Service Propulsion System engine + 16 × R-4D reaction-control thrusters |
| Propellant | NTO / Aerozine 50 |
| Top Speed | 39,897 km/h (24,776 mph) |
| Missions / Launches | 15+ |
| Reusability | Expendable |
🛰️ Notable Missions
- Apollo 8 — first humans to orbit the Moon, December 1968
- Apollo 11 — first crewed Moon landing, July 1969
- Apollo 13 — crew saved after in-flight explosion, April 1970
- Skylab 2-4 — ferried America's first station crews, 1973-1974
- Apollo-Soyuz — final flight, first international docking, July 1975
The Apollo Command and Service Module was the spacecraft that carried every Apollo crew to the Moon and back. Built by North American Aviation for NASA, the 11-metre, 30-tonne two-part vehicle flew three astronauts on missions of up to two weeks — and on the way home from the Moon it hit speeds no humans have matched since: Apollo 10’s crew returned at 39,897 km/h in May 1969, still the all-time record.
It was really two machines in one. The cone-shaped Command Module held the crew, the controls, and the heat shield — the only part that came home. Behind it, the cylindrical Service Module carried the big engine, propellant, oxygen, and the fuel cells that made electricity and drinking water.
Between 1968 and 1975 the CSM flew fifteen crewed missions without ever failing to bring its crew back — including one mission, Apollo 13, where it towed its crippled self home with the crew sheltering in the attached lunar lander.
Development History
NASA ordered the spacecraft in 1961, within months of President Kennedy’s Moon commitment, and development was brutal. The early Block I design was rushed and flawed; during a launch rehearsal on January 27, 1967, a fire in the pure-oxygen cabin of Apollo 1 killed Gus Grissom, Ed White, and Roger Chaffee on the pad.
The 21-month redesign that followed produced the Block II spacecraft: a fireproofed cabin, a quick-opening hatch, and thousands of engineering fixes. It was this rebuilt machine that flew every crewed mission, starting with Apollo 7’s 11-day shakedown in Earth orbit in October 1968.
Confidence grew astonishingly fast. Just two crewed flights in, Apollo 8 rode a Saturn V to lunar orbit in December 1968 — the first time humans left Earth’s gravitational neighborhood — and seven months later Apollo 11’s CSM Columbia waited overhead while Armstrong and Aldrin walked on the Sea of Tranquility.
Design & Capabilities
The Command Module was a 3.9-metre-wide cone with about 6 cubic metres of living space for three astronauts — cozier than a minivan. Its ablative heat shield charred away on purpose during reentry, soaking up temperatures near 2,800 °C at lunar-return speeds before parachutes dropped the capsule into the Pacific.
The Service Module’s single AJ10-137 engine — the Service Propulsion System — delivered about 91 kN and had one non-negotiable job: burning the crew into lunar orbit and, above all, back out of it. It used hypergolic propellants that ignite on contact, eliminating an ignition system that could fail 380,000 km from help. Sixteen R-4D thrusters in four quads handled steering, and three fuel cells combined hydrogen and oxygen for power.
Fully fueled for a lunar mission, the CSM weighed about 30.3 tonnes. On the later J-missions (Apollo 15-17), a bay in the Service Module carried cameras and sensors that mapped the Moon from orbit, plus a small satellite to release.
Notable Missions
Apollo 8 proved the spacecraft could carry humans to the Moon and back. Apollo 11 made history in July 1969. Apollo 13 in April 1970 became the design’s sternest test: an oxygen tank in the Service Module exploded halfway to the Moon, and the Command Module — powered down to a cold lifeboat’s companion — still executed a flawless reentry at journey’s end, bringing all three astronauts home.
After the Moon program ended, the CSM kept working. It ferried three crews to the Skylab station in 1973-74, including a record 84-day mission, and made its final flight in July 1975, docking with a Soviet Soyuz in the Apollo-Soyuz Test Project — a handshake in orbit that closed the space race era.
Frequently Asked Questions
Why did Apollo need two separate modules?
Mass. Every kilogram returning to Earth needs heat shielding and parachutes, so engineers kept the returning part — the Command Module — as small as possible and packed everything expendable into the Service Module behind it: engine, tanks, fuel cells, oxygen. The Service Module was cut loose minutes before reentry and burned up, having done its job.
How fast did the Apollo CSM travel?
Coming home from the Moon, the spacecraft fell into Earth’s gravity and hit about 39,900 km/h — 11 km every second. Apollo 10 holds the official crewed speed record at 39,897 km/h, set in May 1969. No astronauts have gone faster since, because no humans have returned from the Moon since Apollo 17 in December 1972.
Did the Command Module ever land on the Moon?
No. The CSM always stayed in lunar orbit with one astronaut aboard while the other two descended in the separate Lunar Module. The Command Module lacked landing legs and carried far too little propellant to land and relaunch. Its job was the journey — outbound cruise, lunar orbit operations, and the fiery ride home.
How many Apollo CSMs flew with crews?
Fifteen: Apollo 7 through 17 (eleven missions), three Skylab ferry flights in 1973-74, and the Apollo-Soyuz mission in 1975. Several more flew uncrewed tests between 1966 and 1968. Every crewed flight brought its astronauts home safely — a record that survived even the Apollo 13 explosion, thanks to margins built deep into the design.