View source for SR-91 Aurora

{|{{Infobox Aircraft Begin 
  |name = SR-91 "Aurora"
  |image = Image:Aurora2.jpg
  |caption = 
}}{{Infobox Aircraft Type
  |type = Strategic Reconnaissance Aircraft
  |manufacturer = [[Rubin Design Aerospace]]
  |designer =
  |first flight = 2007
  |introduced = 
  |retired = 
  |status = Testing
  |primary user =U.S. Air Force
  |more users = [[International Space Agency]]
  |developed from= SR-71 Blackbird <br> North American X-15 <br> XB-70 Valkyrie 
  |produced = 2007 to present
  |number built = 7
  |unit cost = Unknown
}}
|}

The '''Rubin Design SR-91''' is an advanced, high-altitude strategic reconnaissance aircraft developed by [[Rubin Design Aerospace|Rubin Design Defense Systems]] for use by the United States Air Force. It provides day and night, high-altitude (120,000 feet ASL and above), all-weather surveillance. The aircraft is also being developed for future use in satellite calibration, and satellite data validation.
==History==

==Design and operational details==
===Air inlets===
===Fuselage===
===Stealth===
===Fuel===
===Life support===
===Sensors and payloads===

==Operational history==

==Variants==

==Specifications==
[[Image:Aurora spyplane 3-view.jpg|300px|right]]
{{aircraft specifications/switch
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|plane or copter?=plane
|jet or prop?=jet

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|crew=2 (1 pilot, 1 reconnaissance systems officer)
|length main=115&nbsp;ft
|length alt=35&nbsp;m
|span main=65&nbsp;ft
|span alt=20&nbsp;m
|height main=19&nbsp;ft
|height alt=6&nbsp;m
|area main=3,200 ft²
|area alt=300 m²
|empty weight main=65,000 lb
|empty weight alt=29,480 kg
|loaded weight main=
|loaded weight alt=
|max takeoff weight main=157,000 lb
|max takeoff weight alt=71,215 kg

|engine (jet)=Pratt & Whitney J58-1
|type of jet= afterburning turbojets
|number of jets=4
|thrust main= 32,500 lbf
|thrust alt=267 kN est.
|more general= '''High Speed Powerplant:''' 4× ramjets, scramjets or pulse detonation engines (267 kN est. thrust) each

|max speed main=unknown at sea level
|max speed alt=Mach 10 at altitude
|max speed more=
|range main=9,320&nbsp;mi
|range alt=15,000&nbsp;km
|ceiling main=131,000&nbsp;ft
|ceiling alt=40,000&nbsp;m
|climb rate main=
|climb rate alt=
|loading main=
|loading alt=
|thrust/weight=0.70 est.}}
===Fuel types===
*JP-7 or JP-8 
*Methane, MCH, LH<sub>2</sub> or hydrogen fuel cells.
*Possible use of liquid oxygen and hydrogen oxides.
*Possible use of MHD ([[Wikipedia:Magnetohydrodynamics|Magnetohydrodynamics]]) technology.

===Other equipment===
*Cameras
*IR sensors
*Other advanced recon sensors