The Saturn C-8 was the largest member of the Saturn series of rockets to be designed. It was a potential alternative to the Nova rocket, should NASA have chosen a direct-landing method of lunar exploration for the Apollo program. The first stage was an increased diameter version of the S-IC. The second stage was an increased diameter S-II stage. Both of these stages had eight engines, as opposed to the standard five.
| Attributes | Values |
|---|---|
| rdfs:comment |
|
| foaf:name |
|
| foaf:depiction | |
| country origin | |
| diameter (μ) |
|
| height (μ) |
|
| mass (g) |
|
| rocket function | |
| number of rocket stages |
|
| status |
|
| thumbnail |