View source for Jupiter 246-B

{{Infobox rocket
  |image = 
  |caption = 

  |name = Jupiter 246-B
  |function = Manned launch vehicle
  |country-origin = United States

  |height = 362 ft
  |diameter = 
  |mass = 
  |stages = 2
  |capacities =
  {{Infobox Rocket/Payload
    |location = LEO (241&nbsp;km x 29°)
    |mass = 
  }}

  |family = [[Shuttle Derived Launch Vehicle|SDLV]]
  |comparable = [[National Launch System]]

  |status = Active
  |sites = [[Wikipedia:Kennedy Space Center Launch Complex 39|LC-39]], [[Wikipedia:Kennedy Space Center|Kennedy Space Center]]
  |launches = 
  |payloads = [[Orion spacecraft|Orion Crew Exploration Vehicle]]<br>[[Altair spacecraft|Altair Lunar Surface Access Module]]

  |stagedata =
  {{Infobox Rocket/Stage
    |type       =  booster
    |name       =  [[Wikipedia:Space Shuttle Solid Rocket Booster|Shuttle RSRM]]
    |number     =  2
    |engines    =  1 [[solid-fuel rocket|solid]]
    |thrust     =   (sea level - vacuum)
    |total      =   (sea level - vacuum)
    |SI         =  237.0 - 269.1 sec (sea level - vacuum)
    |burntime   =  123.8 sec
    |fuel       =  [[Wikipedia:Ammonium Perchlorate Composite Propellant|APCP]]/[[Wikipedia:Polybutadiene acrylonitrile|PBAN]]
  }}
  {{Infobox Rocket/Stage
    |type       =  stage
    |stageno    =  First
    |name       =  Common core stage
    |diameter   =  
    |engines    =  4 SSME-Block-II
    |thrust     =   (sea level - vacuum)
    |SI         =  361.4 (SL)<br/>452.2 sec (sea level - vacuum)
    |burntime   =  384.1 sec
    |fuel       =  LOX/LH2
  }}
  {{Infobox Rocket/Stage
    |type       =  stage
    |stageno    =  Second
    |name       =  Jupiter Upper Stage
    |diameter   =  
    |engines    =  6 [[Wikipedia:RL10#Current design|RL10B-2]]
    |thrust     =   (vacuum) 
    |SI         =  459 sec (vacuum)
    |burntime   =  609.9 sec
    |fuel       =  LOX/LH2
  }}
}}