MIflyer
Captain
I think that technically the XP-55 was not a canard because the forward control surface was an elevator and not a wing.
Anyway, too bad they never put a jet engine in it.
Anyway, too bad they never put a jet engine in it.
Curtiss xp-55 Ascender
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johnbr
2nd Lieutenant
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johnbr
2nd Lieutenant
Nice shots!
Peter Gunn
Master Sergeant
Was looking through this thread without signing in and, well, let's just say this happened...
I'm not judging mind you, just...
I'm not judging mind you, just...
Was looking through this thread without signing in and, well, let's just say this happened...
I'm not judging mind you, just...
View attachment 556580
What's on your browsing history???
Hahahahaha!
Peter Gunn
Master Sergeant
And probably best not in a public forum...A rather weighty subject for discussion...
at6
1st Sergeant
On the one hand, they do have loads of personality.Was looking through this thread without signing in and, well, let's just say this happened...
I'm not judging mind you, just...
View attachment 556580
P-39 Expert
Non-Expert
I believe the correct terminology is "junk in the trunk".
WJPearce
Airman 1st Class
A formation of heavies.
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johnbr
2nd Lieutenant
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johnbr
2nd Lieutenant
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johnbr
2nd Lieutenant
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johnbr
2nd Lieutenant
Aircraft disposition
42-78845: crashed during vertical dive on Nov 15, 1943. Pilot bailed out.
42-78846: on display at the Air Zoo in Kalamazoo, Michigan. It is on long-term loan from the Smithsonian's National Air and Space Museum in Washington, D.C.
42-78847: crashed during air show at Wright Field, Ohio on May 27, 1945. Pilot killed.
General characteristics
Crew: One (pilot)
Length: 29 ft 7 in (9.02 m)
Wingspan: 40 ft 7 in (12.37 m)
Height: 10 ft 0 in (3.05 m)
Wing area: 235 sq ft (21.8 m2)
Empty weight: 6,354 lb (2,882 kg)
Gross weight: 7,710 lb (3,497 kg)
Max takeoff weight: 7,930 lb (3,597 kg)
Powerplant: 1 × Allison V-1710-95 liquid-cooled V12 engine, 1,275 hp (951 kW)
Performance
Maximum speed: 390 mph (630 km/h, 340 kn) at 19,300 feet (5,900 m)
Range: 635 mi (1,022 km, 552 nmi)
Service ceiling: 34,600 ft (10,500 m)
Wing loading: 32.8 lb/sq ft (160 kg/m2)
Power/mass: 0.16 hp/lb
Armament
Guns: 4 × 0.50 in (12.7 mm) machine guns in the nose
42-78845: crashed during vertical dive on Nov 15, 1943. Pilot bailed out.
42-78846: on display at the Air Zoo in Kalamazoo, Michigan. It is on long-term loan from the Smithsonian's National Air and Space Museum in Washington, D.C.
42-78847: crashed during air show at Wright Field, Ohio on May 27, 1945. Pilot killed.
General characteristics
Crew: One (pilot)
Length: 29 ft 7 in (9.02 m)
Wingspan: 40 ft 7 in (12.37 m)
Height: 10 ft 0 in (3.05 m)
Wing area: 235 sq ft (21.8 m2)
Empty weight: 6,354 lb (2,882 kg)
Gross weight: 7,710 lb (3,497 kg)
Max takeoff weight: 7,930 lb (3,597 kg)
Powerplant: 1 × Allison V-1710-95 liquid-cooled V12 engine, 1,275 hp (951 kW)
Performance
Maximum speed: 390 mph (630 km/h, 340 kn) at 19,300 feet (5,900 m)
Range: 635 mi (1,022 km, 552 nmi)
Service ceiling: 34,600 ft (10,500 m)
Wing loading: 32.8 lb/sq ft (160 kg/m2)
Power/mass: 0.16 hp/lb
Armament
Guns: 4 × 0.50 in (12.7 mm) machine guns in the nose
The reports are interesting. I always wondered if they had extended the fuselage with a plug behind the pilot big enough for a turbocharger similar to the P-47's. I'd think (with my just enough to get me in trouble aerodynamics knowledge) that would, along with increasing the area of the elevators till they were more actually canards, also help the stall characteristics.
Really though I can't help but wonder if the best thing that could have happened to it was a pair of J-35's in place of the V-1710 with the plug used for them and fuel.
Really though I can't help but wonder if the best thing that could have happened to it was a pair of J-35's in place of the V-1710 with the plug used for them and fuel.
Thumpalumpacus
Lieutenant Colonel
Jettison the canopy, jettison the prop ... but what about that air intake? You better have some strong legs to get out of that SoB.
bail-out was usually done to the side. On most aircraft this was to avoid hitting the tail.
wuzak
Captain
Actually it was during stall tests.
The aircraft flipped on its back and fell to the ground in a flat orientation, but inverted. There was no forward speed, so the control surfaces were ineffective.
Pilot was able to bail out only after the aircraft fell many thousands of feet.
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