This page serves as a repository for overall diagrams of the Jupiter missile.

This diagram of the Jupiter missile has call-outs for the major components. The diagram is labelled "ABMA Dwg J-711-A" with a date of "24 Feb '59".

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From the page 5 of the Redstone Arsenal History Office's HTML version of History of the Jupiter Missile System; Redstone's history web site has been down for several years.
Clean-up by heroicrelics.

The call-outs on this diagram include

• Power Unit
  • Rocket Engine (150,000 lbs. thrust)
    (Engine capable of swivel 7° in any direction)
  • LOX Tank
  • Fuel Line
  • Fuel Tank (RP-1)
• Body Unit
  • Aft Unit
    • Spatial Attitude Control Nozzles (8)
    • Spin Rockets (2)
    • Vernier Engine (500 lbs thrust)
    • Guidance & Control Compartment
  • Nose Cone