| Apollo command and service module | Applications | Crewed cislunar flight and lunar orbit Skylab crew shuttle Apollo–Soyuz Test Project | 1.00 | infobox |
| Apollo command and service module | Batteries | 3 × 40 ampere-hour silver zinc battery | 1.00 | infobox |
| Apollo command and service module | Built | 35 | 1.00 | infobox |
| Apollo command and service module | Burn time | 750 s | 1.00 | infobox |
| Apollo command and service module | Country of origin | United States | 1.00 | infobox |
| Apollo command and service module | Crew capacity | 3 | 1.00 | infobox |
| Apollo command and service module | Design life | 14 days | 1.00 | infobox |
| Apollo command and service module | Designer | Maxime Faget | 1.00 | infobox |
| Apollo command and service module | Diameter | 12.8 ft (3.9 m) | 1.00 | infobox |
| Apollo command and service module | Dry mass | 26,300 lb (11,900 kg) | 1.00 | infobox |
| Apollo command and service module | Failed | 2 | 1.00 | infobox |
| Apollo command and service module | Flown with | Apollo Lunar Module | 1.00 | infobox |
| Apollo command and service module | Last launch | July 15, 1975; 51 years ago (1975-07-15) (Apollo–Soyuz) | 1.00 | infobox |
| Apollo command and service module | Last retirement | July 24, 1975; 51 years ago (1975-07-24) | 1.00 | infobox |
| Apollo command and service module | Launch mass | 32,390 lb (14,690 kg) Earth orbit 63,500 lb (28,800 kg) Lunar | 1.00 | infobox |
| Apollo command and service module | Launched | 19 | 1.00 | infobox |
| Apollo command and service module | Length | 36.2 ft (11.0 m) | 1.00 | infobox |
| Apollo command and service module | Lost | 1 | 1.00 | infobox |
| Apollo command and service module | Maiden launch | February 26, 1966; 60 years ago (February 26, 1966) (AS-201) | 1.00 | infobox |
| Apollo command and service module | Manufacturer | North American Aviation | 1.00 | infobox |
| Apollo command and service module | Maximum thrust | 91.19 kN (20,500 lbf) | 1.00 | infobox |
| Apollo command and service module | Operational | 19 | 1.00 | infobox |
| Apollo command and service module | Operator | NASA | 1.00 | infobox |
| Apollo command and service module | Payload capacity | 2,320 lb (1,050 kg) | 1.00 | infobox |
| Apollo command and service module | Power | 3 × 1.4 kW, 30 V DC fuel cells | 1.00 | infobox |
| Apollo command and service module | Powered by | 1 × AJ10-137 | 1.00 | infobox |
| Apollo command and service module | Propellant | .mw-parser-output .template-chem2-su{display:inline-block;font-size:80%;line-height:1;vertical-align:-0.35em}.mw-parser-output .template-chem2-su>span{display:block;text-align:l… | 1.00 | infobox |
| Apollo command and service module | Regime | Low Earth orbit Cislunar space Lunar orbit | 1.00 | infobox |
| Apollo command and service module | Spacecraft type | Capsule | 1.00 | infobox |
| Apollo command and service module | Specific impulse | 314.5 s (3.084 km/s) | 1.00 | infobox |
