Martin XB-27: Difference between revisions
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{{short description|American bomber project}} |
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__NOTOC__ |
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{{Refimprove|date=June 2019}} |
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{|{{Infobox aircraft begin |
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{{Infobox aircraft |
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|name = XB-27 |
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| name = XB-27 |
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|image = <!-- in the ''File:filename'' format with no image tags. In-flight images are preferred for aircraft. --> |
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| image = XB-27-Schematics.jpg |
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|caption = <!-- Image caption; if it isn't descriptive, please skip. --> |
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| caption = <!-- Image caption; if it isn't descriptive, please skip. --> |
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| alt = <!-- Alt text for main image --> |
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}}{{Infobox aircraft type |
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|type = High-altitude medium bomber |
| type = High-altitude medium bomber |
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| national_origin = [[United States]] |
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|manufacturer = [[Glenn L. Martin Company |
| manufacturer = [[Glenn L. Martin Company]] |
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|designer = <!--Only appropriate for single designers, not project leaders--> |
| designer = <!--Only appropriate for single designers, not project leaders--> |
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| first_flight = <!--If this hasn't happened, skip this field!--> |
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| introduction = <!--Date the aircraft entered or will enter military or revenue service--> |
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|retired = <!--Date the aircraft left service. If vague or more than a few dates, skip this --> |
| retired = <!--Date the aircraft left service. If vague or more than a few dates, skip this --> |
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|status = <!--In most cases, redundant; use sparingly--> |
| status = <!--In most cases, redundant; use sparingly--> |
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| primary_user = <!-- List only one user; for military aircraft, this is a nation or a service arm. Please DON'T add those tiny flags, as they limit horizontal space. --> |
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| more_users = <!-- Limited to THREE (3) 'more users' here (4 total users). Separate users with <br />. --> |
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|produced = <!--Years in production (eg. 1970–1999) if still in active use but no longer built --> |
| produced = <!--Years in production (eg. 1970–1999) if still in active use but no longer built --> |
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| number_built = <!-- Total number of flight-worthy aircraft completed. --> |
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|program cost = <!--Total program cost--> |
| program cost = <!--Total program cost--> |
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|unit cost = <!--Incremental or flyaway cost for military or retail price for commercial aircraft--> |
| unit cost = <!--Incremental or flyaway cost for military or retail price for commercial aircraft--> |
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| developed_from = [[Martin B-26 Marauder]]<!--The aircraft which formed the basis for this aircraft--> |
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|variants |
| variants = <!--Variants OF this aircraft--> |
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| developed_into = <!--For derivative aircraft based on this aircraft--> |
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The '''Martin XB-27''' ('''Martin Model 182''') was an aircraft proposed by the [[Glenn L. Martin Company]] to fill a strong need in the [[United States Army Air Corps]] for a high-altitude [[medium bomber]]. Its design was based approximately on that of Martin's own [[Martin B-26 Marauder|B-26 Marauder]]. The XB-27 |
The '''Martin XB-27''' ('''Martin Model 182''') was an aircraft proposed by the [[Glenn L. Martin Company]] to fill a strong need in the [[United States Army Air Corps]] for a high-altitude [[medium bomber]]. Its design was based approximately on that of Martin's own [[Martin B-26 Marauder|B-26 Marauder]]. The XB-27 remained on paper, and no prototypes were built. |
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==Specifications (as designed)== |
==Specifications (as designed)== |
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{{Aircraft specs |
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{{aircraft specifications |
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|ref=<ref name="Heyman">{{cite book |last1=Heyman |first1=Jos |title=UNITED STATES MILITARY AIRCRAFT : Air Force : B=Bomber |date=2015}}</ref> |
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|plane or copter?=plane |
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|prime units?=imp |
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|jet or prop?=prop |
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<!-- |
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|ref={{Citation needed|date=August 2011}} |
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General characteristics |
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--> |
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|crew=7 |
|crew=7 |
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|capacity= |
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|length main=60 ft 9 in |
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|length |
|length m= |
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|length ft=60 |
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|span main=84 ft 0 in |
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|length in=9 |
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|span alt=25.6 m |
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|length note= |
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|height main=20 ft 0 in |
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|span m= |
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|height alt=6.10 m |
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|span ft=84 |
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|span in=0 |
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|height ft=20 |
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|empty weight main= |
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|height in=0 |
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|empty weight alt= |
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|height note= |
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|loaded weight main=33,000 lb |
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|wing area sqm= |
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|loaded weight alt=15,000 kg |
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|wing area sqft= |
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|max takeoff weight main= |
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|wing area note= |
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|max takeoff weight alt= |
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|swept area sqm=<!-- swing-wings --> |
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|number of props=2 |
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|swept area sqft=<!-- swing-wings --> |
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|engine (prop)=[[Pratt & Whitney R-2800]]-9 |
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|swept area note= |
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|type of prop=[[radial engine]]s |
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|volume m3=<!-- lighter-than-air --> |
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|power main=2,000 hp |
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|volume ft3=<!-- lighter-than-air --> |
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|power alt=1,500 kW |
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|volume note= |
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|performance header=Performance (estimated) |
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|aspect ratio=<!-- sailplanes --> |
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|max speed main=280 mph |
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|airfoil= |
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|max speed alt=450 km/h |
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|empty weight kg= |
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|range main=2,900 mi |
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|empty weight lb= |
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|range alt=4,600 km |
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|empty weight note= |
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|ceiling main=33,500 ft |
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|gross weight kg= |
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|ceiling alt=10,200 m |
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|gross weight lb= |
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|gross weight note= |
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|max takeoff weight kg= |
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|loading main= |
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|max takeoff weight lb= |
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|loading alt= |
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|max takeoff weight note= |
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|power/mass main=0.12 hp/lb |
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|fuel capacity= |
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|power/mass alt=200 W/kg |
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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= |
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<!-- |
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Powerplant |
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--> |
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|eng1 number=2 |
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|eng1 name=[[Pratt & Whitney R-2800-9]] |
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|eng1 type= |
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|eng1 kw=<!-- prop engines --> |
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|eng1 hp=<!-- prop engines --> |
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|eng1 shp=2000 |
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|prop blade number=4 |
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|prop name=constant-speed propellers |
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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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<!-- |
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Performance |
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--> |
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|max speed mph=280 |
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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=2900 |
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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 ft=33500 |
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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={{cvt|0.12|hp/lb}} |
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|thrust/weight= |
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|more performance= |
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<!-- |
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Armament |
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--> |
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|guns=<br> |
|guns=<br> |
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** 3 × .30 |
** 3 × {{cvt|.30|in}} [[machine gun]]s |
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** 1 × . |
** 1 × {{cvt|.30|in}} machine gun |
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|bombs=> |
|bombs=>{{cvt|4000|lb}} |
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}} |
}} |
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==References== |
==References== |
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{{Reflist}} |
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{{commonscat|Glenn L. Martin Company}} |
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*[http://www.nationalmuseum.af.mil/factsheets/factsheet.asp?id=2573 USAF Museum] |
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{{Martin aircraft}} |
{{Martin aircraft}} |
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{{USAF bomber aircraft}} |
{{USAF bomber aircraft}} |
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{{aviation lists}} |
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[[Category:United States bomber aircraft 1940–1949|Martin B-27]] |
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[[Category:Martin aircraft|B-27]] |
[[Category:Martin aircraft|B-27]] |
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[[Category:1940s United States bomber aircraft|Martin B-27]] |
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[[Category:Twin piston-engined tractor aircraft]] |
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{{aero-1940s-stub}} |
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[[Category:High-wing aircraft]] |
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[[Category:Aircraft with retractable tricycle landing gear]] |
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[[Category:Cancelled military aircraft projects of the United States]] |
Latest revision as of 01:36, 11 November 2024
This article needs additional citations for verification. (June 2019) |
XB-27 | |
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General information | |
Type | High-altitude medium bomber |
National origin | United States |
Manufacturer | Glenn L. Martin Company |
History | |
Developed from | Martin B-26 Marauder |
The Martin XB-27 (Martin Model 182) was an aircraft proposed by the Glenn L. Martin Company to fill a strong need in the United States Army Air Corps for a high-altitude medium bomber. Its design was based approximately on that of Martin's own B-26 Marauder. The XB-27 remained on paper, and no prototypes were built.
Specifications (as designed)
[edit]Data from [1]
General characteristics
- Crew: 7
- Length: 60 ft 9 in (18.52 m)
- Wingspan: 84 ft 0 in (25.60 m)
- Height: 20 ft 0 in (6.10 m)
- Powerplant: 2 × Pratt & Whitney R-2800-9 , 2,000 shp (1,500 kW) each
- Propellers: 4-bladed constant-speed propellers
Performance
- Maximum speed: 280 mph (450 km/h, 240 kn)
- Range: 2,900 mi (4,700 km, 2,500 nmi)
- Service ceiling: 33,500 ft (10,200 m)
- Power/mass: 0.12 hp/lb (0.20 kW/kg)
Armament
- Guns:
- 3 × .30 in (7.6 mm) machine guns
- 1 × .30 in (7.6 mm) machine gun
- Bombs: >4,000 lb (1,800 kg)
See also
[edit]Related development
Aircraft of comparable role, configuration, and era
Related lists
References
[edit]- ^ Heyman, Jos (2015). UNITED STATES MILITARY AIRCRAFT : Air Force : B=Bomber.