词条 | Culver XPQ-15 | |||||||||||||||||||||||||
释义 |
The Culver XPQ-15, also known as the XTD3C-1, was an American target drone developed by the Culver Aircraft Company late in World War II. Design and developmentThe XPQ-15 was a low-wing monoplane of conventional design. It was powered by a Franklin O-405 opposed piston engine.[1] Design work began in 1943.[2] Operational historyFour examples of the XPQ-15 were built for evaluation by the United States Army Air Forces in 1945; two additional aircraft were tested by the United States Navy as the XTD3C-1. No production contract was placed.[1] Variants
USAAF variant; four produced.[1]
USN variant; two produced, BuNos 29665-29666.[3] Specifications (XPQ-15){{Aircraft specs|ref=Parsch [1] |prime units?=imp |genhide=Y |crew= |capacity= |length m= |length ft= |length in= |length note= |span m= |span ft= |span in= |span note= |height m= |height ft= |height in= |height note= |wing area sqm= |wing area sqft= |wing area note= |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=1 |eng1 name=Franklin O-405 |eng1 type=opposed piston engine |eng1 kw= |eng1 hp=200 |eng1 note= |power original= |more power= |prop blade number= |prop name= |prop dia m= |prop dia ft= |prop dia in= |prop note= |max speed kmh= |max speed mph=220 |max speed kts= |max speed note= |max speed mach= |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= |range km= |range miles= |range nmi= |range note= |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 m= |ceiling ft= |ceiling note= |g limits= |roll rate= |glide ratio= |climb rate ms= |climb rate ftmin= |climb rate note= |time to altitude= |lift to drag= |wing loading kg/m2= |wing loading lb/sqft= |wing loading note= |fuel consumption kg/km= |fuel consumption lb/mi= |power/mass= |more performance= |avionics= }} References
1. ^1 2 3 Parsch 2009 2. ^Mingos 1946, p.318. 3. ^Grossnick and Armstrong 1997, p.540.
External links{{commons category|Culver XPQ-15}}
6 : Culver aircraft|United States special-purpose aircraft 1940–1949|Single-engined tractor aircraft|Low-wing aircraft|Target drones of the United States|Aircraft first flown in 1945 |
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