Editing Messerschmitt Me 163 Komet (section)

==Specifications: Me 163B-1a==
[[File:Messerschmitt Me 163 3-view.svg|thumb|Messerschmitt Me 163B 3-view drawings]]
{{Aircraft specs
|ref= ''The Warplanes of the Third Reich'',<ref name=Green>{{cite book |last1 = Green |first1 = William |last2 = Punnett |first2 = Dennis (With line drawings by) |title = The Warplanes of the Third Reich |date = 1970 |publisher = Doubleday |location = Garden City, N.Y. |isbn = 0385057822 |pages = 594–606}}</ref> ''Profile No225: Messerschmitt Me 163 Komet''<ref name="Bateson">{{cite journal |last1 = Bateson |first1 = Richard P. |last2 = Spate |first2 = Wolfgang |title = Messerschmitt Me 163 Komet |journal = Aircraft in Profile |date = 1971 |issue = 225}}</ref>
|prime units?= met
<!--
General characteristics
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|crew= 1
|capacity= (Me 163S + 1)
|length m= 5.7
|span m= 9.3
|height m= 2.5
|wing area sqm= 19.6
|aspect ratio=<!-- sailplanes -->
|airfoil=
|empty weight lb= 4,200
|gross weight kg=
|gross weight lb=
|gross weight note=
|max takeoff weight lb= 9,500
|fuel capacity=<br/>
** '''''[[C-Stoff]]''''' (fuel) {{cvt|468|kg}}
** '''''[[T-Stoff]]''''' (oxidizer) {{cvt|1550|kg}}
|more general=
<!--
Powerplant
-->
[[File:Plan view of a Messerschmitt Me 163 Komet.jpg|thumb|Plan view of the un-restored Messerschmitt Me 163 Komet at the Smithsonian Institute's Udvar-Hazy Center in Chantilly, Virginia, USA.]]
|eng1 number= 1
|eng1 name= [[Hellmuth Walter Kommanditgesellschaft]] [[HWK 109-509A-2]]
|eng1 type= bi-propellant liquid-fuelled rocket motor
|eng1 lbf= 3,307
|eng1 note= maximum; {{cvt|220|lbf|order=flip}} minimum, fully variable
<!--
Performance
-->
|max speed kmh=
|max speed mph=
|max speed kts=
|max speed note=
|max speed mach=<!-- supersonic aircraft -->
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh= 900
|never exceed speed note= at all altitudes, sea level to {{cvt|12000|m}}{{clarify|The often quoted top speed of {{convert|596|mi/h|km/h|abbr=on}} up to the tropopause is impossible, as it corresponds to a Mach Number of over .89—the Me 163B ran into severe compressibility above .82 and complete loss of control at M=.84. This anomaly has not been explained, although it might relate to uncompensated instrumentation on the operational aircraft.|date=December 2017}}<br/>
* '''Flap limiting speed:''' {{cvt|300|km/h|mph kn}}
* '''Rotate speed at take-off:''' {{cvt|280|km/h|mph kn}}
* '''Best climbing speed:''' {{cvt|700|-|720|km/h|mph kn}}
|endurance= 7.5 mins powered
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|glide ratio=<!-- sailplanes -->
|climb rate ftmin= 16,000
|time to altitude= From standing start<br/>
** {{cvt|2000|m}} in 1.48 min
** {{cvt|4000|m}} in 2.02 min
** {{cvt|6000|m}} in 2.27 min
** {{cvt|8000|m}} in 2.54 min
** {{cvt|10000|m}} in 3.19 min
** {{cvt|12000|m}} in 3.45 min
|sink rate ms=<!-- sailplanes -->
|sink rate ftmin=<!-- sailplanes -->
|sink rate note=
|lift to drag=
|wing loading kg/m2= 209
|wing loading note= at maximum take-off weight
|fuel consumption kg/km=
|fuel consumption lb/mi=
|thrust/weight= 0.42
|more performance=
<!--
Armament
-->
|guns=<br/>
** 2 × {{cvt|30|mm|3}} Rheinmetall Borsig [[MK 108 cannon]] with 60 rpg

}}