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S-II + Interstage + Aft Interstage (Outdated)

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The S-II was the second stage of the Saturn V rocket. It was built by North American Aviation. Using liquid hydrogen (LH2) and liquid oxygen (LOX) it had five J-2 engines in a quincunx pattern. The second stage accelerated the Saturn V through the upper atmosphere with 1,000,000 pounds-force (4,400 kN) of thrust.

From Wikipedia

General Characteristics

  • Created On iOS
  • Wingspan 22.9ft (7.0m)
  • Length 27.1ft (8.2m)
  • Height 49.2ft (15.0m)
  • Empty Weight 71,619lbs (32,486kg)
  • Loaded Weight 92,247lbs (41,842kg)

Performance

  • Power/Weight Ratio 2.192
  • Wing Loading 53.1lbs/ft2 (259.5kg/m2)
  • Wing Area 1,735.7ft2 (161.3m2)
  • Drag Points 91571

Parts

  • Number of Parts 1570
  • Control Surfaces 0
  • Performance Cost 2,647