Editing Blohm & Voss BV 155 (section)

==Specifications (BV 155B)==
{{Aircraft specs
|ref=<ref name="Greenaottr">Green 2010, pp. 148–152.</ref>
|prime units?=met<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, met(ric) first for all others. You MUST choose a format, or no specifications will show -->
<!--
        General characteristics
-->
|genhide=

|crew=1
|length m=12
|span m=20.5
|height m=3
|wing area sqm=39
|empty weight kg=4,870
|gross weight kg=5,520
|gross weight note=Proposal A<br />
::::{{convert|5,125|kg|lb|abbr=on|0}} Proposal B
::::{{convert|5,100|kg|lb|abbr=on|0}} Proposal C
::::{{convert|5,440|kg|lb|abbr=on|0}} Proposal D
|max takeoff weight kg=6,020
|fuel capacity={{convert|1,200|L|impgal|abbr=on|0}}
<!--
        Powerplant
-->
|eng1 number=1
|eng1 name=[[Daimler-Benz DB 603A]]
|eng1 type=inverted V-12 liquid-cooled piston engine with [[TKL 15]] turbo-charger
|eng1 kw=1,200
|eng1 note=for take-off<br />
::::{{convert|1,200|kW|hp|abbr=on|0}} at {{convert|10,000|m|ft|abbr=on}}
::::{{convert|1,081|kW|hp|abbr=on|0}} at {{convert|15,000|m|ft|abbr=on}}

|prop blade number=4
|prop name=constant speed paddle bladed propeller
<!--
        Performance
-->
|max speed kmh=420
|max speed note=at sea level<br />
::::{{convert|520|km/h|mph|abbr=on|0}} at {{convert|6,000|m|ft|abbr=on}}
::::{{convert|600|km/h|mph|abbr=on|0}} at {{convert|10,000|m|ft|abbr=on}}
::::{{convert|650|km/h|mph|abbr=on|0}} at {{convert|12,000|m|ft|abbr=on}}
::::{{convert|690|km/h|mph|abbr=on|0}} at {{convert|16,000|m|ft|abbr=on}}
|range km=460
|range note=at maximum continuous power with {{convert|595|L|impgal|abbr=on|0}} of fuel at sea level<br />
::::{{convert|560|km|mi|abbr=on|0}} with {{convert|595|L|impgal|abbr=on|0}} of fuel at {{convert|10,000|m|ft|abbr=on}}
::::{{convert|590|km|mi|abbr=on|0}} with {{convert|595|L|impgal|abbr=on|0}} of fuel at {{convert|16,000|m|ft|abbr=on}}
::::{{convert|1,080|km|mi|abbr=on|0}} with {{convert|1,200|L|impgal|abbr=on|0}} of fuel at sea level
::::{{convert|1,350|km|mi|abbr=on|0}} with {{convert|1,200|L|impgal|abbr=on|0}} of fuel at {{convert|10,000|m|ft|abbr=on}}
::::{{convert|1,440|km|mi|abbr=on|0}} with {{convert|1,200|L|impgal|abbr=on|0}} of fuel at {{convert|16,000|m|ft|abbr=on}}
|ceiling m=16,950
|ceiling note=service ceiling<br />
*'''Maximum ceiling''' {{convert|17,100|m|ft|abbr=on}}
|climb rate ms=11.5
|climb rate note=initial<br />
::::{{convert|3.92|m/s|ft/s|abbr=on|0}} at {{convert|16,000|m|ft|abbr=on}}
|time to altitude= {{convert|16,000|m|ft|abbr=on}} in 29 minutes
<!--
        Armament
-->
|guns=<br />
::'''Proposal A'''
:::* 1 × {{convert|30|mm|in|abbr=on|3}} [[MK 108 cannon]] as an engine mounted ''Motorkanone'' firing through the propeller shaft{{Citation needed|date=December 2011}}
:::* 2 × 20 mm [[MG 151 cannon|MG 151/20 cannon]]
::'''Proposal B'''
:::* 1 × {{convert|30|mm|in|abbr=on|3}} [[MK 103 cannon]] as an engine mounted ''Motorkanone'' firing through the propeller shaft with 60 rounds
:::* 2 × {{convert|15|mm|in|abbr=on|3}} [[MG 151 cannon]] with 200 rpg
::'''Proposal C'''
:::* 3 × {{convert|30|mm|in|abbr=on|3}} [[MK 108 cannon]] with 60 rpg.
::'''Proposal D'''
:::* 3 × {{convert|30|mm|in|abbr=on|3}} [[MK 103 cannon]] with 60 rpg (two mounted in under-wing fairings).
}}