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Saturn C
The Saturn C series study oversaw the evolution of a heavy launch vehicle that would eventually become the Saturn V. Only the Saturn C-1 and C-5 variants actually flew, as Saturn I and Saturn V respectively.
Saturn C-2 is a four-stage launch vehicle using an S-I first stage with eight H-1 engines and an S-II second stage using four J-2 engines (a smaller variant of the five engine S-II used on Saturn V). The RL10 powered S-IV makes up the third stage and the rocket is topped by Centaur D (S-V stage).
Saturn C-3B features a widened S-IB-2 first stage tank with two or three F-1 engines, and the same S-II and S-IV stages as the C-2. The C-3N features a nuclear NERVA engine in the third stage.
Saturn C-4 consists of three stages: an S-IB-4 first stage with four F-1 engines, the S-II second stage, and J-2 powered S-IVB third stage. The C-5 adds a fifth J-2 to the S-II stage, finalising the configuration that would become the Saturn V launch vehicle.
Tags: Sarnus
Launch Vehicle | First Stage | Boosters | Second Stage | Third Stage |
---|---|---|---|---|
Saturn C-2 | Sarnus S-I (8x H-1) | S-II (4x J-2) | S-IV (6x RL10) | S-V (Centaur D) |
Saturn C-3B | Sarnus S-IB-2 (2/3x F-1) | S-II | S-IV | |
Saturn C-3N | Sarnus S-IB-2 | S-II | S-IVN (1x NERVA) | |
Saturn C-4 | Sarnus S-IB-4 (4x F-1) | S-II | S-IVB (1x J-2) |
From top to bottom
- S-V (Centaur D)
- S-IV
- S-IVB
- S-IVN
- S-II
- S-I
- S-IB
- 0.9375m
- 1.25m
- 1.5m
- 1.875m
- 2.5m
- 3.125m
- 3.75m
- 5.625m