Mil V-7

Mil V-7

Company type	Experimental aircraft
Industry	Aerospace
Founded	Late 1950s
Headquarters	Soviet Union
Products	Experimental helicopter

Template:Infobox aircraft The Mil V-7 was an experimental aircraft featuring a four-seat configuration and powered by AI-7 ramjet engines mounted at the tips of its dual rotor blades. Its design included an egg-shaped main fuselage, skid-type landing gear, and a two-blade tail rotor attached to a short tubular tail boom. Although four units were constructed during the late 1950s, only one is documented to have achieved flight, carrying solely the pilot.

Specifications

{{Aircraft specs |ref=The Osprey Encyclopaedia of Russian Aircraft 1875–1995 |prime units?=met |genhide=

|crew=1 |capacity=3 passengers |length m= |length ft= |length in= |dia m= |dia ft= |dia in= |width m= |width ft= |width in= |height m= |height ft= |height in= |empty weight kg=730 |empty weight lb= |gross weight kg=835 |gross weight lb= |max takeoff weight kg= |max takeoff weight lb= |more general= |eng1 number=2 |eng1 name=Ivchenko AI-7 |eng1 type=ramjets |eng1 kw= |eng1 hp= |eng1 shp= |eng1 kn= |eng1 lbf=123.5 |power original= |thrust original= |eng1 kn-ab= |eng1 lbf-ab= |more power=

|rot number=1 |rot dia m=11.6 |rot dia ft= |rot dia in= |rot area sqm= |rot area sqft= |perfhide=y

|max speed kmh= |max speed mph= |max speed kts= |cruise speed kmh= |cruise speed mph= |cruise speed kts= |range km= |range miles= |range nmi= |endurance= |ceiling m= |ceiling ft= |g limits= |roll rate= |max climb rate ms= |max climb rate ftmin= |max lift-to-drag ratio= |max disk loading kg/m2= |max disk loading lb/sqft= |}

See also

• List of experimental aircraft