Lafayette1 at 04:52, 9 July 2016

2016-07-09T04:52:24Z

Lafayette1: Created page with "{{Infobox rocket |image = |caption = |name = Jupiter 246-B |function = Manned launch vehicle |country-origin = United States |height = 362 ft |diameter =..."

2016-07-09T04:52:00Z

Created page with "{{Infobox rocket |image = |caption = |name = Jupiter 246-B |function = Manned launch vehicle |country-origin = United States |height = 362 ft |diameter =..."

New page

{{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 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
}}
}}

The '''Jupiter 200''' is an American [[Wikipedia:human-rated|human-rated]] [[Wikipedia:Shuttle-Derived Launch Vehicle|Space Shuttle-derived]] heavy [[Wikipedia:expendable launch system|expendable launch vehicle]] originally used by the [[International Space Agency]] (ISA) as part of the [[Phoenix Program]]. Currently, the Saturn V is the tallest, heaviest, and most powerful rocket ever brought to operational status, supporting all manned launches beyond [[Wikipedia:low Earth orbit|low Earth orbit]].

A modified version of the Jupiter 246 proposed by [[Wikipeida:DIRECT|DIRECT]] and originally introduced as the ''Jupiter 246-B'', the Jupiter 200 is derived from existing Space Shuttle components and has been upgraded since its introduction in 2010 to improve safety and performance.

@@ Line 10: / Line 10: @@
    |diameter =
    |mass =
-   |stages = 2
+   |stages = 3
    |capacities =
    {{Infobox Rocket/Payload
@@ Line 29: / Line 29: @@
      |type       =  booster
      |name       =  [[Wikipedia:Space Shuttle Solid Rocket Booster|Shuttle RSRM]]
-     |number     =  2
+     |number     =  4
      |engines    =  1 [[solid-fuel rocket|solid]]
      |thrust     =   (sea level - vacuum)

Jupiter (rocket) - Revision history

Lafayette1 at 04:52, 9 July 2016

Lafayette1: Created page with "{{Infobox rocket |image = |caption = |name = Jupiter 246-B |function = Manned launch vehicle |country-origin = United States |height = 362 ft |diameter =..."