Martin P7M SubMaster

{{Refimprove|date=September 2018}}

{{Infobox Aircraft Begin

|name = P7M

|caption =

|image =

}}{{Infobox Aircraft Type

|type = anti-submarine warfare (ASW) flying boat

|manufacturer = Glenn L. Martin Company

|designer =

|first flight =

|introduced =

|retired =

|status =

|primary user = United States Navy

|more users =

|produced =

|number built = 0 (mock-up only)

|unit cost =

|program cost =

|variants with their own articles =

|developed from=P5M Marlin

}}

The Martin P7M was an unbuilt aircraft designed by the Glenn L. Martin Company in the 1950s. The design was initiated to meet a requirement of the United States Navy for an anti-submarine warfare flying boat.

Design and development

The design was for a flying boat that would make use of boundary layer control (BLC) to achieve slow speed flight. It was intended that this would enable the aircraft to land on the open ocean in rough seas and deploy a dipping sonar. Martin proposed a variant of the P5M Marlin, the P5M-3, to take advantage of this phenomenon.

Martin continued development of the P5M-3 under the designation P7M Submaster, introducing two General Electric J85 BLC gas generators, one in the rear of each outer engine nacelle. A mock-up was built, but the P7M, Convair XP6Y and Grumman G-132 were all cancelled when the U.S. Navy abandoned its open-ocean seaplane requirement.{{Cite book |last=Johnson |first=E.R. |url=https://archive.org/details/americanflyingbo0000john/page/349 |title=American flying boats and amphibious aircraft : an illustrated history |date=2009 |publisher=McFarland & Co. |isbn=978-0786439744 |location=Jefferson, N.C. |pages=349–353}}

Specifications (P7M projected)

{{Aircraft specs

|ref=

|prime units?=imp

|genhide=

|crew=

|capacity=

|length ft=136

|span ft=111

|span in=7

|height ft=39

|wing area sqft=2500

|aspect ratio=

|airfoil=

|empty weight kg=

|empty weight lb=

|empty weight note=

|gross weight kg=

|gross weight lb=

|gross weight note=

|max takeoff weight kg=

|max takeoff weight lb=

|max takeoff weight note=

|fuel capacity=

|more general=

|eng1 number=4

|eng1 name=Wright R-1820-42

|eng1 type=radial piston engines

|eng1 kw=

|eng1 hp=1525

|eng1 note=

|eng2 number=2

|eng2 name=General Electric YJ85-GE-1

|eng2 type=turbojet

|eng2 kn=

|eng2 lbf=

|eng2 note=gas generators for BLC in rear of outer nacelles

|more power=

|prop blade number=

|prop name=

|prop dia m=

|prop dia ft=

|prop dia in=

|prop note=

|perfhide=

|max speed kts=350

|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=

|never exceed speed mph=

|never exceed speed kts=

|never exceed speed note=

|minimum control speed kmh=

|minimum control speed mph=

|minimum control speed kts=

|minimum control speed note=

|range nmi=1200

|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=

|ceiling ft=25,300

|ceiling note=service ceiling

|g limits=

|roll rate=

|glide ratio=

|climb rate ms=

|climb rate ftmin=

|climb rate note=

|time to altitude=

|sink rate ms=

|sink rate ftmin=

|sink rate note=

|lift to drag=

|wing loading kg/m2=

|wing loading lb/sqft=

|wing loading note=

|fuel consumption kg/km=

|fuel consumption lb/mi=

|power/mass=

|thrust/weight=

|more performance=

|armament=* Missiles, bombs, and depth charges on external hard-points

|guns=

|bombs=

|rockets=

|missiles=

|hardpoints=

|hardpoint capacity=

|hardpoint rockets=

|hardpoint missiles=

|hardpoint bombs=

|hardpoint other=

|avionics=

}}

References