American orbital launch vehicle. Boeing study, 1967. Configuration of improved Saturn 5 with Titan UA1207 120 inch solid rocket boosters. Saturn IC stretched 336 inches with 6.0 million pounds propellant and 5 F-1 engines; Saturn II and Saturn IVB stages strengthened but not stretched. Empty mass of stages increased by 13.9% (S-IC), 8.6% (S-II) and 11.8% (S-IVB). Studied again by Boeing in 1967 as Saturn V-4(S)B.
Status: Study 1967. Payload: 171,990 kg (379,170 lb). Thrust: 69,317.10 kN (15,583,104 lbf). Gross mass: 4,699,860 kg (10,361,410 lb). Height: 89.00 m (291.00 ft). Diameter: 10.06 m (33.00 ft). Apogee: 185 km (114 mi).
LEO Payload: 171,990 kg (379,170 lb) to a 185 km orbit at 28.00 degrees. Payload: 63,160 kg (139,240 lb) to a translunar trajectory. Flyaway Unit Cost 1985$: 97.440 million.
Stage Data - Saturn MLV-V-4(S)-B
Stage 0. 4 x Titan UA1207. Gross Mass: 319,330 kg (704,000 lb). Empty Mass: 51,230 kg (112,940 lb). Thrust (vac): 7,116.999 kN (1,599,965 lbf). Isp: 272 sec. Burn time: 120 sec. Isp(sl): 245 sec. Diameter: 3.05 m (10.00 ft). Span: 3.05 m (10.00 ft). Length: 34.14 m (112.00 ft). Propellants: Solid. No Engines: 1. Engine: UA1207. Status: In Production.
Stage 1. 1 x Saturn MS-IC-1. Gross Mass: 2,694,703 kg (5,940,803 lb). Empty Mass: 169,719 kg (374,166 lb). Thrust (vac): 45,948.754 kN (10,329,691 lbf). Isp: 310 sec. Burn time: 158 sec. Isp(sl): 270 sec. Diameter: 10.06 m (33.00 ft). Span: 19.00 m (62.00 ft). Length: 48.15 m (157.97 ft). Propellants: Lox/Kerosene. No Engines: 5. Engine: F-1A. Status: Study NASA 1966. Comments: Basic Saturn IC stretched 240 inches with F-1A engines uprated 20% in thrust and 6 second improvement in specific impulse.
Stage 2. 1 x Saturn MS-II-1-J-2T-250K. Gross Mass: 521,447 kg (1,149,593 lb). Empty Mass: 49,877 kg (109,959 lb). Thrust (vac): 5,558.310 kN (1,249,558 lbf). Isp: 441 sec. Burn time: 348 sec. Isp(sl): 290 sec. Diameter: 10.06 m (33.00 ft). Span: 10.06 m (33.00 ft). Length: 25.88 m (84.90 ft). Propellants: Lox/LH2. No Engines: 5. Engine: J-2T-250K. Status: Study NASA 1966. Comments: Basic Saturn II with 41 inch stretch of hydrogen tank, uprated J-2T 250k engines with 25% improvement in thrust and 16 second increase in specific impulse.
From : astronautix
GENERAL INFO
- Predecessor: Moonlab(mobile friendly)
- Successors 1 craft(s)
- Created On: Android
- Game Version: 0.9.506.0
- Price: $-1,975,872k
- Number of Parts: 629
- Dimensions: 114 m x 16 m x 16 m
PERFORMANCE
- Total Delta V: 38.2km/s
- Total Thrust: 92.9MN
- Engines: 43
- Wet Mass: 2.67E+6kg
- Dry Mass: -96,731,856kg
STAGES
| Stage | Engines | Delta V | Thrust | Burn | Mass |
|---|---|---|---|---|---|
| 1 | 14 | 35.3km/s | 55.5MN | 2.1m | 2.67E+6kg |
| 2 | 0 | 0m/s | 0N | 0s | 2.19E+6kg |
| 3 | 8 | 1m/s | 1.0MN | 1s | 1.01E+6kg |
| 4 | 5 | 2.9km/s | 11.6MN | 2.5m | 1.01E+6kg |
2 Comments
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4,265 kittman3.7 years ago
very nice! I am gonna look for a nice heavy satellite or craft and blast it into LDO orbit. I think this thing could handle a lot of stuff! If I am doing my math correctly, this thing will launch 190 tons of cargo into LEO?
also, when jettisoning the side boosters, I cant help but notice there is some similarity to the Soyuz Korelev Cross. pretty cool!
Hello! very good Craft, congratulations !. Have you noticed that the N-1, the second largest rocket in the world, also has many variants? Here is a link to Astronautix.com so you can see the different types if you are interested. http://www.astronautix.com/n/n1.html