Editing Bachem Ba 349 Natter (section)

==Specifications (Ba 349B-1)==
[[File:Bachem Ba 349a Natter.svg|thumb|Ba 349]]
{{Aircraft specs
|ref= ''Aircraft of the Third Reich''<ref name="Greenaottr">{{cite book |last = Green |first = William |title = Aircraft of the Third Reich |publisher = Aerospace Publishing Limited |location = London |year = 2010 |edition = 1st |page = 34 |isbn = 978-1-900732-06-2}}</ref>
|prime units? = met

|crew= 1
|length m= 6
|length ft=
|length in=
|length note=
|span m= 4
|span ft=
|span in=
|span note=
|dia m=
|dia ft=
|dia in=
|dia note=
|height m= 2.25
|height ft=
|height in=
|height note= (without fins)
|wing area sqm= 4.7
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg= 880
|empty weight lb=
|empty weight note= fuel expended
|gross weight kg= 2,232
|gross weight lb=
|gross weight note=<br/>
* '''Gross weight boosters jettisoned:''' {{convert|1,769|kg|lb|abbr=on|0}}
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity= 650 kg
|more general=

|eng1 number= 1
|eng1 name= [[Walter HWK 109-509C-1]]
|eng1 type= bi-fuel rocket engine
|eng1 kn= 11.2
|eng1 note= ''Hauptofen'' main chamber<br>
::::: {{convert|2.9|kN|lbf|abbr=on|0}} ''Marschofen'' auxiliary chamber

|eng2 number= 4
|eng2 name= [[Schmidding SG 34]]
|eng2 type= solid fuel booster rockets
|eng2 kn= 4.9
|eng2 lbf=
|eng2 note=<br>
::::: or 2 x {{convert|9.8|kN|lbf|abbr=on|0}} solid fuel booster rocket motors

|more power=

|max speed kmh= 1,000
|max speed mph=
|max speed kts=
|max speed note= at {{convert|5,000|m|ft|abbr=on|0}}
|max speed mach=
|cruise speed kmh= 800
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|range km= 60
|range miles=
|range nmi=
|range note= after climb at {{convert|3,000|m|ft|abbr=on|0}}<br/>
:::: {{convert|55|km|mi|abbr=on|0}}after climb at {{convert|6,000|m|ft|abbr=on|0}}
:::: {{convert|42|km|mi|abbr=on|0}}after climb at {{convert|9,000|m|ft|abbr=on|0}}
:::: {{convert|40|km|mi|abbr=on|0}}after climb at {{convert|10,000|m|ft|abbr=on|0}}
|combat range km=
|combat range miles=
|combat range nmi=
|combat range note=
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry range note=
|endurance= 4.36 minutes at {{convert|6,000|m|ft|abbr=on|0}}<br/>
:::: 3.15 minutes at {{convert|9,000|m|ft|abbr=on|0}}
|ceiling m= 12,000
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms= 190
|climb rate ftmin=
|climb rate note=
|time to altitude= 62 seconds to {{convert|12|km|abbr=on}}
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|thrust/weight=

|more performance=

|armament=
* 24 × {{convert|73|mm|in|abbr=on|3}} [[Henschel Hs 297]] Föhn 73mm{{Sfn | Munson | 1978 | p =  28}} rocket shells
* or 33 × {{convert|55|mm|in|abbr=on|3}} [[R4M]] rocket shells
* or 2 × {{convert|30|mm|in|abbr=on|3}} [[MK 108]] cannon with 30 rpg (proposed)
}}