Grigorovich M-19: Difference between revisions
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The '''Grigorovich M-19''' was a reconnaissance flying boat designed by Grigorovich in the late 1910s. |
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{|{{Infobox aircraft begin |
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| name=M-19 |
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| image= |
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| caption= |
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}}{{Infobox aircraft type |
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| type= |
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| national origin=[[Russia]] |
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| manufacturer=Grigorovich |
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| designer= |
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| first flight= |
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| introduced= |
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| retired= |
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| status= |
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| primary user= |
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| more users= <!--Limited to three in total; separate using <br /> --> |
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| produced= <!--years in production--> |
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| number built= |
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| program cost= <!--Total program cost--> |
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| unit cost= <!--Incremental or flyaway cost for military or retail price for commercial aircraft--> |
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| developed from= |
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| variants with their own articles= |
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}} |
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The '''Grigorovich M-19''' was a reconnaissance flying boat designed by Grigorovich in the late 1910s. The M-19 was a [[Grigorovich M-9]] modified to be of the same size as the [[Grigorovich M-15]]. Assembly of the prototype was started in 1918, but the aircraft was not completed.<ref name=Shavrov>{{cite book |last=Shavrov |first=V.B. |title=Istoriia konstruktskii samoletov v SSSR, 1938–1950 |year=1994 |publisher=Mashinostroenie |location=Moscow |isbn=978-5-217-00477-5 |edition=gg. (3 izd.) |language=Russian |pages=292–293}}</ref> |
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==Design== |
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<!-- ==Development== --> |
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The M-19 was a [[Grigorovich M-9]] modified to be of the same size as the [[Grigorovich M-15]]. Assembly of the prototype was started in 1918, but the aircraft was not built.<ref>Shavrov, 1985."History of aircraft construction in the USSR", Vol.1 p.292-293</ref> |
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<!-- ==Operational history== --> |
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==Specifications (M-19)== |
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{{Aircraft specs |
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|ref=<ref name="ramm-19">{{cite web |title=M-19, D.P.Grigorovich |url=http://ram-home.com/ram-old/m-19.html |website=Russian Aviation Museum |accessdate=2 February 2019}}</ref> |
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|prime units?=met |
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General characteristics |
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|crew= |
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==Specifications== |
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{{aircraft specifications |
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|plane or copter?=plane |
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|jet or prop?=prop |
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If an item doesn't apply, like capacity, leave it blank. For instructions on using |more general=, |more performance=, |power original=, and |thrust original= see [[Template talk:Aircraft specifications]]. To add a new line, end the old one with a right parenthesis ")" and start a new, fully formatted line beginning with * --> |
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|ref=<ref>http://ram-home.com/ram-old/m-19.html</ref> |
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|crew=2 |
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|capacity= |
|capacity= |
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|length |
|length m=8.5 |
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|length |
|length ft= |
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|length in= |
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|span main=13 m |
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|length note= |
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|span m=13 |
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|height main= |
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|span ft= |
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|span in= |
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|area main=48.0 m² |
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|span note= |
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|upper span m= |
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|upper span ft= |
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|upper span in= |
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|upper span note= |
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|mid span m= |
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|mid span ft= |
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|mid span in= |
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|mid span note= |
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|lower span m= |
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|lower span ft= |
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|lower span in= |
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|lower span note= |
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|swept m=<!-- swing-wings --> |
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|swept ft=<!-- swing-wings --> |
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|swept in=<!-- swing-wings --> |
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|swept note= |
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|dia m=<!-- airships etc --> |
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|dia ft=<!-- airships etc --> |
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|dia in=<!-- airships etc --> |
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|dia note= |
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|width m=<!-- if applicable --> |
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|width ft=<!-- if applicable --> |
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|width in=<!-- if applicable --> |
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|width note= |
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|height m= |
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|height ft= |
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|height in= |
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|height note= |
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|wing area sqm=48 |
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|wing area sqft= |
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|wing area note= |
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|swept area sqm=<!-- swing-wings --> |
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|swept area sqft=<!-- swing-wings --> |
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|swept area note= |
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|volume m3=<!-- lighter-than-air --> |
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|volume ft3=<!-- lighter-than-air --> |
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|volume note= |
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|aspect ratio=<!-- sailplanes --> |
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|airfoil= |
|airfoil= |
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|empty weight |
|empty weight kg= |
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|empty weight |
|empty weight lb= |
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|empty weight note= |
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|gross weight kg= |
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|gross weight lb= |
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|useful load main= kg |
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|gross weight note= |
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|useful load alt= kg |
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|max takeoff weight |
|max takeoff weight kg= |
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|max takeoff weight |
|max takeoff weight lb= |
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|max takeoff weight note= |
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|fuel capacity= |
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|lift kg=<!-- lighter-than-air --> |
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|lift lb=<!-- lighter-than-air --> |
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|lift note= |
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|more general= |
|more general= |
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<!-- |
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|engine (prop)=Salmson |
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Powerplant |
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|type of prop=pusher |
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--> |
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|number of props=1 |
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|eng1 number=1 |
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|power main= kW |
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|eng1 name=[[Salmson radial engine]] |
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|power alt=160 hp |
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|eng1 type=9-cylinder water-cooled radial piston engine |
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|eng1 kw=<!-- prop engines --> |
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|eng1 hp=160 |
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|eng1 shp=<!-- prop engines --> |
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|eng1 kn=<!-- jet/rocket engines --> |
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|eng1 lbf=<!-- jet/rocket engines --> |
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|eng1 note= |
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|power original= |
|power original= |
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|thrust original= |
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|max speed main= km/h |
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|eng1 kn-ab=<!-- afterburners --> |
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|max speed alt= knots, mph |
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|eng1 lbf-ab=<!-- afterburners --> |
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|cruise speed main= km/h |
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|cruise speed alt= knots, mph |
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|eng2 number= |
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|stall speed main= km/h |
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|eng2 name= |
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|stall speed alt= knots, mph |
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|eng2 type= |
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|never exceed speed main= km/h |
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|eng2 kw=<!-- prop engines --> |
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|never exceed speed alt= knots, mph |
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|eng2 hp=<!-- prop engines --> |
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|range main= km |
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|eng2 shp=<!-- prop engines --> |
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|range alt= |
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|eng2 kn=<!-- jet/rocket engines --> |
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|ceiling main= m |
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|eng2 lbf=<!-- jet/rocket engines --> |
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|ceiling alt= ft |
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|eng2 note= |
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|climb rate main= m/s |
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|eng2 kn-ab=<!-- afterburners --> |
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|climb rate alt= ft/min |
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|eng2 lbf-ab=<!-- afterburners --> |
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|loading main= kg/m² |
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|loading alt= lb/ft² |
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|eng3 number= |
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|eng3 name= |
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|eng3 type= |
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|eng3 kw=<!-- prop engines --> |
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|eng3 hp=<!-- prop engines --> |
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|eng3 shp=<!-- prop engines --> |
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|eng3 kn=<!-- jet/rocket engines --> |
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|eng3 lbf=<!-- jet/rocket engines --> |
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|eng3 note= |
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|eng3 kn-ab=<!-- afterburners --> |
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|eng3 lbf-ab=<!-- afterburners --> |
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|more power= |
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|prop blade number=<!-- propeller aircraft --> |
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|prop name= |
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|prop dia m=<!-- propeller aircraft --> |
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|prop dia ft=<!-- propeller aircraft --> |
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|prop dia in=<!-- propeller aircraft --> |
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|prop dia note= |
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|rot number=<!-- helicopters --> |
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|rot dia m=<!-- helicopters --> |
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|rot dia ft=<!-- helicopters --> |
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|rot dia in=<!-- helicopters --> |
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|rot area sqm=<!-- helicopters --> |
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|rot area sqft=<!-- helicopters --> |
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|rot area note= |
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<!-- |
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Performance |
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--> |
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|perfhide= |
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|max speed kmh= |
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|max speed mph= |
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|max speed kts= |
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|max speed note= |
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|max speed mach=<!-- supersonic aircraft --> |
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|cruise speed kmh= |
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|cruise speed mph= |
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|cruise speed kts= |
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|cruise speed note= |
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|stall speed kmh= |
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|stall speed mph= |
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|stall speed kts= |
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|stall speed note= |
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|never exceed speed kmh= |
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|never exceed speed mph= |
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|never exceed speed kts= |
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|never exceed speed note= |
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|minimum control speed kmh= |
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|minimum control speed mph= |
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|minimum control speed kts= |
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|minimum control speed note= |
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|range km= |
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|range miles= |
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|range nmi= |
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|range note= |
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|combat range km= |
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|combat range miles= |
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|combat range nmi= |
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|combat range note= |
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|ferry range km= |
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|ferry range miles= |
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|ferry range nmi= |
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|ferry range note= |
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|endurance=<!-- if range unknown --> |
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|ceiling m= |
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|ceiling ft= |
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|ceiling note= |
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|g limits=<!-- aerobatic --> |
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|roll rate=<!-- aerobatic --> |
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|glide ratio=<!-- sailplanes --> |
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|climb rate ms= |
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|climb rate ftmin= |
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|climb rate note= |
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|time to altitude= |
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|sink rate ms=<!-- sailplanes --> |
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|sink rate ftmin=<!-- sailplanes --> |
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|sink rate note= |
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|lift to drag= |
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|wing loading kg/m2= |
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|wing loading lb/sqft= |
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|wing loading note= |
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|disk loading kg/m2= |
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|disk loading lb/sqft= |
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|disk loading note= |
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|fuel consumption kg/km= |
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|fuel consumption lb/mi= |
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|power/mass= |
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|thrust/weight= |
|thrust/weight= |
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|power/mass main= W/kg |
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|power/mass alt= hp/lb |
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|more performance= |
|more performance= |
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<!-- |
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|armament= |
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Armament |
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|avionics= |
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--> |
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|armament=<!-- add bulletted list here or if you want to use the following |
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specific parameters, remove this parameter--> |
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|guns= |
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|bombs= |
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|rockets= |
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|missiles= |
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|hardpoints= |
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|hardpoint capacity= |
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|hardpoint rockets= |
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|hardpoint missiles= |
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|hardpoint bombs= |
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|hardpoint other= |
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|avionics= |
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}} |
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{{reflist}} |
{{reflist}} |
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==Bibliography== |
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{{commons category|Grigorovich M-19}} |
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*{{cite journal |last1=Kulikov|first1=Victor|title=Le fascinante histoire des hydravions de Dimitry Grigorovitch|journal=Avions: Toute l'aéronautique et son histoire |date=December 1996 |issue=45 |pages=20–33 |trans-title=The Fascinating History of the Seaplanes of Dimitry Grigorovitch|language=French |issn=1243-8650}} |
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<!-- ==External links== --> |
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{{Grigorovich aircraft}} |
{{Grigorovich aircraft}} |
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[[Category:Single-engined pusher aircraft]] |
[[Category:Single-engined pusher aircraft]] |
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[[Category:Flying boats]] |
[[Category:Flying boats]] |
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[[Category:Russian military reconnaissance aircraft |
[[Category:1910s Russian military reconnaissance aircraft]] |
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[[Category:Biplanes]] |
[[Category:Biplanes]] |
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[[Category:Grigorovich aircraft|M-19]] |
[[Category:Grigorovich aircraft|M-19]] |
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Latest revision as of 14:33, 20 January 2021
| M-19 | |
|---|---|
| Role | |
| National origin | Russia |
| Manufacturer | Grigorovich |
The Grigorovich M-19 was a reconnaissance flying boat designed by Grigorovich in the late 1910s. The M-19 was a Grigorovich M-9 modified to be of the same size as the Grigorovich M-15. Assembly of the prototype was started in 1918, but the aircraft was not completed.[1]
Specifications (M-19)
[edit]Data from [2]
General characteristics
- Length: 8.5 m (27 ft 11 in)
- Wingspan: 13 m (42 ft 8 in)
- Wing area: 48 m2 (520 sq ft)
- Powerplant: 1 × Salmson radial engine 9-cylinder water-cooled radial piston engine, 120 kW (160 hp)
Performance
References
[edit]- ^ Shavrov, V.B. (1994). Istoriia konstruktskii samoletov v SSSR, 1938–1950 (in Russian) (gg. (3 izd.) ed.). Moscow: Mashinostroenie. pp. 292–293. ISBN 978-5-217-00477-5.
- ^ "M-19, D.P.Grigorovich". Russian Aviation Museum. Retrieved 2 February 2019.