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Jupiter 246-B - Revision history
2026-05-23T07:46:06Z
Revision history for this page on the wiki
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http://www.lafayetteinc.com/index.php?title=Jupiter_246-B&diff=3097&oldid=prev
Lafayette1: Created page with "{{Infobox rocket |image = |caption = |name = Jupiter 246-B |function = Manned launch vehicle |country-origin = United States |height = 362 ft |diameter =..."
2016-07-09T04:29:07Z
<p>Created page with "{{Infobox rocket |image = |caption = |name = Jupiter 246-B |function = Manned launch vehicle |country-origin = United States |height = 362 ft |diameter =..."</p>
<p><b>New page</b></p><div>{{Infobox rocket<br />
|image = <br />
|caption = <br />
<br />
|name = Jupiter 246-B<br />
|function = Manned launch vehicle<br />
|country-origin = United States<br />
<br />
|height = 362 ft<br />
|diameter = <br />
|mass = <br />
|stages = 2<br />
|capacities =<br />
{{Infobox Rocket/Payload<br />
|location = LEO (241&nbsp;km x 29°)<br />
|mass = <br />
}}<br />
<br />
|family = [[Shuttle Derived Launch Vehicle|SDLV]]<br />
|comparable = [[National Launch System]]<br />
<br />
|status = Active<br />
|sites = [[Wikipedia:Kennedy Space Center Launch Complex 39|LC-39]], [[Wikipedia:Kennedy Space Center|Kennedy Space Center]]<br />
|launches = <br />
|payloads = [[Orion spacecraft|Orion Crew Exploration Vehicle]]<br>[[Altair spacecraft|Altair Lunar Surface Access Module]]<br />
<br />
|stagedata =<br />
{{Infobox Rocket/Stage<br />
|type = booster<br />
|name = [[Wikipedia:Space Shuttle Solid Rocket Booster|Shuttle RSRM]]<br />
|number = 2<br />
|engines = 1 [[solid-fuel rocket|solid]]<br />
|thrust = (sea level - vacuum)<br />
|total = (sea level - vacuum)<br />
|SI = 237.0 - 269.1 sec (sea level - vacuum)<br />
|burntime = 123.8 sec<br />
|fuel = [[Wikipedia:Ammonium Perchlorate Composite Propellant|APCP]]/[[Wikipedia:Polybutadiene acrylonitrile|PBAN]]<br />
}}<br />
{{Infobox Rocket/Stage<br />
|type = stage<br />
|stageno = First<br />
|name = Common core stage<br />
|diameter = <br />
|engines = 4 SSME-Block-II<br />
|thrust = (sea level - vacuum)<br />
|SI = 361.4 (SL)<br/>452.2 sec (sea level - vacuum)<br />
|burntime = 384.1 sec<br />
|fuel = LOX/LH2<br />
}}<br />
{{Infobox Rocket/Stage<br />
|type = stage<br />
|stageno = Second<br />
|name = Jupiter Upper Stage<br />
|diameter = <br />
|engines = 6 [[Wikipedia:RL10#Current design|RL10B-2]]<br />
|thrust = (vacuum) <br />
|SI = 459 sec (vacuum)<br />
|burntime = 609.9 sec<br />
|fuel = LOX/LH2<br />
}}<br />
}}</div>
Lafayette1