Editing Lockheed SR-71 Blackbird (section)

==Specifications (SR-71A)==
[[File:Lockheed SR-71A 3view.svg|thumb|right|upright=1.4| SR-71A Blackbird]]
[[File:Lockheed SR-71B trainer model 3view.png|thumb|right|upright=1.4| SR-71B trainer model]]
[[File:Sr-71-composit.gif|350px|thumb|right|upright=1.4|SR-71 epoxy asbestos composite areas]]

{{Aircraft specs
|ref= Lockheed SR-71 Blackbird<ref name=Pace_p110>{{harvp|Pace|2004|p=110}}</ref>
|prime units?=kts
<!--  General characteristics
-->
|crew=2; Pilot and reconnaissance systems officer (RSO)
|length ft=107
|length in=5
|length note=
|span ft=55
|span in=7
|span note=
|height ft=18
|height in=6
|height note=<br/>
*'''Wheel track:''' {{cvt|16|ft|8|in|0}}
*'''Wheelbase:''' {{cvt|37|ft|10|in|0}}
|wing area sqft=1800
|wing area note=
|aspect ratio=1.7
|airfoil=
|empty weight lb=67500
|empty weight note=
|gross weight lb=152000
|gross weight note=
|max takeoff weight lb=172000
|max takeoff weight note=
|fuel capacity={{cvt|12219.2|USgal|impgal l}} in 6 tank groups (9 tanks)
|more general=
<!--  Powerplant
-->
|eng1 number=2
|eng1 name=[[Pratt & Whitney J58]] (JT11D-20J or JT11D-20K)
|eng1 type=afterburning turbojets
|eng1 lbf=25000
|eng1 note=<br/>
::::'''JT11D-20J''' {{cvt|32500|lbf|kN|2}} wet (fixed inlet guidevanes)
::::'''JT11D-20K''' {{cvt|34000|lbf|kN|2}} wet (2-position inlet guidevanes)
<!--  Performance
-->
|max speed kts=1910
|max speed note=at {{cvt|80000|ft}}
|max speed mach=3.3{{refn|Maximum speed limit was Mach 3.2, but could be raised to Mach 3.3 if the engine compressor inlet temperature did not exceed {{convert|801|°F|°C|abbr=on}}.<ref>{{harvp|Graham|2002|pp=93,223}}</ref>|group=N}}
|cruise speed kts=
|cruise speed note=
|stall speed kts=
|stall speed note=
|never exceed speed kts=
|never exceed speed note=
|minimum control speed kts=
|minimum control speed note=
|range nmi=
|range note=
|combat range nmi=
|combat range note=
|ferry range nmi=2824
|ferry range note=
|endurance=<!-- if range unknown -->
|ceiling ft=85000
|ceiling note=
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|glide ratio=<!-- sailplanes -->
|climb rate ftmin=11820
|climb rate note=
|time to altitude=
|sink rate ftmin=<!-- sailplanes -->
|sink rate note=
|lift to drag=
|wing loading lb/sqft=84
|wing loading note=
|fuel consumption lb/mi=
|thrust/weight=0.44

|more performance=
|avionics={{cvt|3500|lb|0}} of mission equipment
:* Itek KA-102A {{cvt|36|-|48|in|mm}} camera
:*[[Signals intelligence|Signals and Electronic Intelligence]] equipment in the following compartments
::* A – nose radar
::* D – right chine bay
::* E – electronics bay
::* K – left forward mission bay
::* L – right forward mission bay
::* M – left forward mission bay
::* N – right forward mission bay
::* P – left aft mission bay
::* Q – right aft mission bay
::* R – radio equipment bay
::* S – left aft mission bay
::* T – right aft mission bay
}}