Auto Credit Based on KirRu's Moonlab(mobile friendly)

American orbital launch vehicle. Boeing study, 1968. Four core vehicles from Saturn V-25(S) study lashed together to obtain million-pound payload using existing hardware. First stage consisted of 4 Saturn IC's stretched 498 inches with 6.64 million pounds propellant and 5 F-1 engines; second stage 4 Saturn II standard length stages with 5 J-2 engines
Status: Study 1968. Payload: 527,600 kg (1,163,100 lb). Thrust: 160,135.00 kN (35,999,780 lbf). Gross mass: 15,504,720 kg (34,182,050 lb). Height: 95.00 m (311.00 ft). Diameter: 10.06 m (33.00 ft). Apogee: 486 km (301 mi).

LEO Payload: 527,600 kg (1,163,100 lb) to a 486 km orbit at 28.00 degrees.

Stage Data - Saturn V-4X(U)

Stage 1. 4 x Saturn MS-IC-25(S). Gross Mass: 3,223,800 kg (7,107,200 lb). Empty Mass: 211,900 kg (467,100 lb). Thrust (vac): 45,925.500 kN (10,324,463 lbf). Isp: 304 sec. Burn time: 192 sec. Isp(sl): 265 sec. Diameter: 10.06 m (33.00 ft). Span: 19.00 m (62.00 ft). Length: 54.70 m (179.40 ft). Propellants: Lox/Kerosene. No Engines: 5. Engine: F-1A. Status: Study Boeing 1967. Comments: S-IC with 41.5 foot stretch, 6,640,0000 lbs propellant, uprated F-1 engines.
Stage 2. 4 x Saturn MS-II-4(S)B. Gross Mass: 494,100 kg (1,089,300 lb). Empty Mass: 42,300 kg (93,200 lb). Thrust (vac): 5,169.000 kN (1,162,037 lbf). Isp: 421 sec. Burn time: 355 sec. Isp(sl): 200 sec. Diameter: 10.06 m (33.00 ft). Span: 10.06 m (33.00 ft). Length: 24.84 m (81.49 ft). Propellants: Lox/LH2. No Engines: 5. Engine: J-2. Status: Study Boeing 1967. Comments: Standard S-II but with structural strength increased from 86% to 502% depending on station, resulting in 8.6% increase in empty weight.
Stage 3. 1 x Saturn MS-II-4(S)B. Gross Mass: 494,100 kg (1,089,300 lb). Empty Mass: 42,300 kg (93,200 lb). Thrust (vac): 5,169.000 kN (1,162,037 lbf). Isp: 421 sec. Burn time: 355 sec. Isp(sl): 200 sec. Diameter: 10.06 m (33.00 ft). Span: 10.06 m (33.00 ft). Length: 24.84 m (81.49 ft). Propellants: Lox/LH2. No Engines: 5. Engine: J-2. Status: Study Boeing 1967. Comments: Standard S-II but with structural strength increased from 86% to 502% depending on station, resulting in 8.6% increase in empty weight.

From : astronautix

GENERAL INFO

  • Predecessor: Moonlab(mobile friendly)
  • Created On: Android
  • Game Version: 0.9.506.0
  • Price: $-1,516,880k
  • Number of Parts: 1656
  • Dimensions: 151 m x 39 m x 39 m

PERFORMANCE

  • Total Delta V: 49.9km/s
  • Total Thrust: 253.5MN
  • Engines: 113
  • Wet Mass: 1.08E+7kg
  • Dry Mass: -143,496,096kg

STAGES

Stage Engines Delta V Thrust Burn Mass
1 40 38.8km/s 179.2MN 2.6m 1.08E+7kg
2 32 1m/s 4.0MN 1s 4.06E+6kg
3 20 3.7km/s 46.3MN 2.8m 4.06E+6kg
5 5 7.4km/s 11.6MN 2.5m 7.33E+5kg

6 Comments

  • Log in to leave a comment
  • Profile image

    I should tell you, I just got a beta for SR2 with an updated physics engine, and I’m finally able to run this leviathan. It handles awkwardly, requiring a fast forward to steer it to a prograde position. Very slow at turning but it gets to orbit :).

    27 days ago
  • Profile image

    Oh god it gets worse

    one month ago
  • Profile image

    What Have you Done? It’s so big it broke my game trying to load it into the physics engine. It hardly could run in the hangar.

    one month ago
  • Profile image

    oh sweet jesus

    one month ago
  • Profile image
    20.1k KirRu

    Damn

    one month ago
  • Profile image
    295 UAviator

    MOAR BOOSTERS

    one month ago

4 Upvotes

Log in in to upvote this post.