Living Person
Saturn_V
is
As of April 19, 2026
59 years old
approximately!
Date of Birth
(1967 ) is
Goat
Year
* Calculated from Wikipedia data.
Accuracy is not guaranteed.
approx.Cosmic Age Calculator
Moon
approx. 793.9 years old
Mercury
approx. 246.6 years old
Venus
approx. 96.5 years old
Mars
approx. 31.6 years old
Jupiter
approx. 5 years old
Saturn
approx. 2 years old
* Calculated based on each planet's orbital period.
 The launch of the Apollo 11 mission on Saturn V SA-506, July 16, 1969 | |
| Function |
|
|---|---|
| Manufacturer | |
| Country of origin | United States |
| Project cost | US$6.4 billion (equivalent to $34.5 billion in 2024) |
| Cost per launch | US$185 million (equivalent to $995 million in 2024) |
| Size | |
| Height | 111 m (363 ft) |
| Diameter | 10 m (33 ft) |
| Mass | 2,822,171 to 2,965,241 kg (6,221,823 to 6,537,238 lb) |
| Stages | 3 |
| Capacity | |
| Payload to LEO | |
| Altitude | 185 km (115 mi) |
| Mass | 140,000 kg (310,000 lb) |
| Payload to TLI | |
| Mass | 43,500 kg (95,900 lb) |
| Associated rockets | |
| Family | Saturn |
| Derivative work | Saturn INT-21 |
| Comparable |
|
| Launch history | |
| Status | Retired |
| Launch sites | Kennedy Space Center, LC-39 |
| Total launches | 13 |
| Success(es) | 12 |
| Partial failure | 1 (Apollo 6) |
| First flight | November 9, 1967 (AS-501 Apollo 4) |
| Last flight | May 14, 1973 (AS-513 Skylab) |
| First stage – S-IC | |
| Height | 42 m (138 ft) |
| Diameter | 10 m (33 ft) |
| Empty mass | 137,000 kg (303,000 lb) |
| Gross mass | 2,214,000 kg (4,881,000 lb) |
| Powered by | 5 × F-1 |
| Maximum thrust | 33,000 kN (7,500,000 lbf) at sea level |
| Specific impulse | 260 s (2.5 km/s) minimum at sea level |
| Burn time | 150 seconds |
| Propellant | LOX / RP-1 |
| Second stage – S-II | |
| Height | 24.87 m (81 ft 7 in) |
| Diameter | 10 m (33 ft) |
| Empty mass | 43,000 kg (95,000 lb) |
| Gross mass | 470,000 kg (1,037,000 lb) |
| Powered by | 5 × J-2 |
| Maximum thrust | 4,400 kN (1,000,000 lbf) in vacuum |
| Specific impulse | 424 s (4.16 km/s) (427 s (4.19 km/s) at 5:1 mixture ratio) |
| Burn time | 395 seconds |
| Propellant | LOX / LH2 |
| Third stage – S-IVB | |
| Height | 17.86 m (58 ft 7 in) |
| Diameter | 6.60 m (21 ft 8 in) |
| Empty mass | 15,200 kg (33,600 lb) |
| Gross mass | 120,500 kg (265,600 lb) |
| Powered by | 1 × J-2 |
| Maximum thrust | 1,000 kN (225,000 lbf) in vacuum |
| Specific impulse | 424 s (4.16 km/s) (427 s (4.19 km/s) at 5:1 mixture ratio) |
| Burn time | 165 + 312 seconds (2 burns) |
| Propellant | LOX / LH2 |
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